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Piper Aircraft Corporation T1040, Maintenance Manual

The Piper Aircraft Corporation T1040 Maintenance Manual is a comprehensive guide for keeping your aircraft in top condition. This manual covers all aspects of maintenance, ensuring that your aircraft operates safely and efficiently. Download the manual for free from manualshive.com and ensure your aircraft is always in top condition.

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VENDOR PUBLICATIONS.

BATTERY:

Gill Lead-Acid Battery
(Teledyne Battery
Products)
Service Manual

= P /N: GSM - 682

SAFT Nickel-Cadmium
Battery Operating and
Maintenance Manual

= P/N: DC 3176-5A

Marathon Nickel
Cadmium
Battery Instruction
Manual

= P/N: BA-89

DE-ICE SYSTEM (PROPELLERS):

B.F. Goodrich
Electrothermal
Propeller Deice
Maintenance Manual

= P/N: 68-04-712 (Latest Revision)

B.F. Goodrich
Electrothermal
Propeller Deice
Installation
and Removal
Procedures

= P/N: 59-728 (Latest Revision)

ENGINE:

PT6A-11/110
Maintenance Manual

= P/N: 3030442

HEATER:

Maintenance and
Overhaul Manual

= P/N: 24E25-1

PROPELLER:

Hartzell Overhaul
Manual

= P/N: 117-D

Hartzell Spinner
Assembly and
Maintenance
Manual

= P/N: 127

5A5

PIPER AIRCRAFT

T-1040

MAINTENANCE MANUAL

Introduction

Page - 4

Revised: July 13, 1984

Summary of Contents for T1040

Page 1: ...MAINTENANCE MANUAL CARD 1OF5 PA 31T3 T1040 PIPER AIRCRAFT CORPORATION PART NUMBER 761765 1A1 Courtesy of Bomar Flying Service www bomar biz...

Page 2: ...ub System Sections Thesesectionsare identified by the secondelementof thestandardizednumberingsystem The number 40 of thebasicnumberseries32 40 00is for the WheelsandBrakes portionof thelandinggear Th...

Page 3: ...list of Charts is for all fiche in this set following list of Illustrations 4 A complete list of paragraph titles and appropriate Grid location numbers is given at the beginning of each Chapter relat...

Page 4: ...3 4 and 5 1 2 3 4 and 5 1 2 3 4 and 5 1 2 3 4 and 5 3 2 1 and 3 INTERIM REVISION Revisions appear in Chapter 5 of card 1 and Chapter 30 or card 3 Please dispose of your current cards 1 and 3 and repla...

Page 5: ...kel Cadmium Battery instruction Manual DE ICE SYSTEM PROPELLERS B F Goodrich Electrothermal Propeller Deice Maintenance Manual B F Goodrich Electrothermal Propeller Deice Installation and Removal Proc...

Page 6: ...Models Lear Siegler Inc Overhaul Manual Series 23048 PIPER PUBLICATIONS PARTS CATALOG P N 8013C P N 23700 P N 23202 761 761 Piper Aircraft Corporation 820 E Bald Eagle Street Lock Haven Pennsylvania...

Page 7: ...7 Air Conditioning System Electronic Leak Detector Autopilot Avionics TIF Instruments 3661 N W 74th Street Miami Florida 33147 305 696 7100 Edo Corporation AvionicsDivision P O Box 610 Municipal Airpo...

Page 8: ...t Akron Ohio 44318 216 374 3895 The B F Goodrich Company 6400 Goldsboro Road Suite 102 Bethesda Maryland 20034 301 229 5000 Leach Corporation 5915 Avalon Boulevard Los Angeles California 90003 213 232...

Page 9: ...eneral Controls 801 Allen Avenue Glendale California 91201 213 842 6131 Aeroquip Corporation Marmon Division 1214 Exposition Boulevard Los Angeles California 90064 213 774 3230 Aerosonic Corporation 1...

Page 10: ...ator Woodward Governor Company Drake and Lemay Roads Fort Collins Colorado 80521 303 482 5811 Auxilec Incorporated One Willow Park Center Farmingdale New York 11735 516 694 1441 Lear Siegler Incorpora...

Page 11: ...F1 10 PARKING ANDMOORING IF5 11 REQUIRED PLACARDS IF8 12 SERVICING 1F13 20 STANDARD PRACTICES AIRFRAME 1G21 21 ENVIRONMENTAL SYSTEM 2B1 22 AUTOFLIGHT 2F1 23 COMMUNICATIONS 2F4 24 ELECTRICAL POWER 2F10...

Page 12: ...4F20 53 FUSELAGE 4G16 55 STABILIZERS 4G19 56 WINDOWS 4H15 57 WINGS 411 61 PROPELLER 4117 70 STANDARD PRACTICES ENGINES 4K5 71 POWERPLANT 4K8 72 ENGINE TURBO PROP 4L1 73 ENGINEFUELSYSTEM 4L4 74 IGNITI...

Page 13: ...Oil CoolerDoors 1G11 12 9 LubricationChart CabinDoor Baggage Door Seats 1G12 12 10 LubricationChart AirConditionerQuillShaft 1G12 20 1 TorqueWrenchExtension 1H1 20 2 CorrectMethodof InstallingRodEndB...

Page 14: ...Drive Plate Removing Bearing _ Installing Pulley and Drive Plate Bearing Installing Pulley and Drive Plate Removing Coil Housing Retaining Ring Positioning Sankyo Compressor Internal Parts Fabricated...

Page 15: ...27 9 Installationof AileronRiggingTool 2J13 27 9a WrappingControlPedestalAileronTrim Drum 2J16 27 10 TrimControlsInstallation 2J17 27 11 AileronControlTravelsandCableTension 2J18 27 12 SafetyWiringCon...

Page 16: ...Pump 3C10 28 15 Test Equipment Hookup 3C15 28 16 Alternate Indicator Bench Test Hookup 3C18 28 17 Fuel Gauge Adjustment 3C19 29 1 Schematic Diagram Hydraulic System 3D20 29 2 Schematic of Power Pack E...

Page 17: ...picalUseof DialIndicator 3H17 30 20 Centering of Brushes on Slip Rings 3H18 30 21 WiringSchematic ElectricPropellerDeicing System 3H18 30 22 ModularBrushAssemblyWearCheck 3H20 30 23 Angleof ContactBru...

Page 18: ...mitSwitch 3L16 32 27 GearWarningSwitchesInstallation 3L16 32 28 NoseGearWearLimits 3L18 32 29 MainGearWearLimits 3L21 33 1 LogoLight AssemblyAdjustments 4B17 34 1 InstrumentAirSystemInstallation Typic...

Page 19: ...ronBalancing 4115 61 1 PropellerInstallation 4122 61 2 TypicalNicksandRemovalMethod 4I23 61 3 PropellerGovernor 4J3 61 4 PropellerSynchrophaserInstallation WoodwardType I 4J5 61 5 PropellerSynchrophas...

Page 20: ...iperJack Part No 18338 00 5H9 95 2 Fabricated TailStand 5H10 95 3 ProtectiveClosuresInstallation 5H11 95 4 FabricatedBellcrankRiggingTool 5H12 95 5 FabricatedAileronand ElevatorRiggingTool 5H13 95 6 F...

Page 21: ...ndicated 2G21 2405 SpecificGravityTemperatureCorrection 2G22 2406 CapacityRatingsat DischargeRates 2G23 2407 ElectrolyteFreezingPoints 2G23 2408 CircuitLoadChart 2H7 2601 Pressure Temperature Correcti...

Page 22: ...902 Troubleshooting PneumaticSystemPressure Gauge 4E5 3903 Troubleshooting EngineOilPressureGauge 4E5 3904 Troubleshooting FuelPressureGauge 4E6 3905 Troubleshooting AirTemperature Gauge 4E9 3906 Trou...

Page 23: ...emCalibrationData 5C21 7702 Digital Analog TorqueCalibrationData 5C23 7703 WestonKuliteTorquePressureIndicating SystemTansducerVoltages 5C24 7901 OilPressureGaugeCalibrationData 5D17 9101 Listof Consu...

Page 24: ...PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL THIS PAGEINTENTIONALLYLEFT BLANK 1A24...

Page 25: ...CHAPTER AIRWORTHINESS LIMITATIONS 1B1...

Page 26: ...IONS TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 4 00 00 AIRWORTHINESS LIMITATIONS 1B3 4 00 01 General 1B3 4 Cont Effec Page 1 Issued March 26 1982 1B2 PIPER AIRC...

Page 27: ...91 163 and 135of the Federal Aviation Regulations NOTE Refer to the LIMITATIONS in the Pilot s Operating Handbook and FAA Approved Flight Manual for a detailed delineation of theflight limitations of...

Page 28: ...CHAPTER TIME LIMITS MAINTENANCE CHECKS 1B4...

Page 29: ...5 21 06 Revisions 1B15 5 21 07 Away From Home Station Requirements 1B 16 5 21 08 Event 1 1B17 5 21 09 Event 2 IC1 2R 11 82 5 21 10 Event 3 1C8 2R 11 82 5 21 11 Event 4 1C15 5 21 12 Special Inspections...

Page 30: ...PECTION If the airplane has been operated so that any of its components have exceeded their maximum operational limits check with the appropriate manufacturer SCHEDULEDMAINTENANCECHECKS CONTINUOUSINSP...

Page 31: ...ulletins are of special importance and should be complied with promptly These are sent to the latest registered owners and Piper Service Representative Service Letters deal with product improvements a...

Page 32: ...nd during inspections will be entered on the Discrepancy Record The person conducting the inspection will advise the Owner and or Operator of the discrepancies found during the inspection and entered...

Page 33: ...the four Events are complete and recorded an entry is made in the Event Record and Cycle Inspection Record which are the running logs or current status of the aircraft inspections Each event will be...

Page 34: ...iled 8 Fuselage Main Detailed 9 Cockpit Routine 10 Lubrication 3 Special Inspections inspections to be performed and recorded with the appropriate Event Inspection 4 Operational Inspection to be perfo...

Page 35: ...e appropriate record 8 Service Publication Compliance Record is used to record the compliance of all manufacturers service publications and contains the following information 1 Name of Manufacturer 2...

Page 36: ...next inspection This ten 10 percent shall only be used to return the aircraft back to the maintenance base when inspection intervals fall due and the aircraft is away from home base 6 Tests Operation...

Page 37: ...in that the system is functioning properly This person will log bench test and operational test in the permanent aircraft records Serviceable parts that were issued to the component will be filed in t...

Page 38: ...fice A duplicate copy should be maintained in this manual Name Address Street City State Zip Telephone Number Any change in personnel responsible for scheduling the inspection program will be added wi...

Page 39: ...of the manufacturer No changes can be made to this Inspection Program unless prior notice is given to the responsible F A A District Office who in turn must approve of the change prior to itsenactmen...

Page 40: ...on this type aircraft The results of the inspection will be noted on the proper Sign Off Sheets which are then brought back to the home base The pilot will be responsible for all inspection forms and...

Page 41: ...and fittings for leaks security chafing dents and cracks 5 Clean and inspect oil radiator cooling fins 6 Remove and inspect oil filter 7 Clean exterior of engine Pratt and Whitney Maintenance Manual 8...

Page 42: ...ck for proper oil level and filler locking cap for security 31 Inspect engine mounts for cracks and loose mount bolts 32 Inspect rubber mount bushings for deterioration 33 Inspect firewall for cracks...

Page 43: ...ING ROUTINE See chapter 57 Maintenance Manual 1 Check surfaces skins and tip for damage and loose rivets 2 Inspect aileron and tab hinges for security of attachment and operation 3 Inspect aileron bal...

Page 44: ...ect actuating cylinder for leaks and security 22 Inspect position indicating switches and electrical wires for condition and security LEFT GEAR 1 Check oleo struts for proper extension Check for prope...

Page 45: ...Clean and inspect up and down lock actuator rod assemblies and rod end bearing assemblies for damage binding corrosion remove boot freedom of movement operation and lubrication 14 Inspect nose gear lo...

Page 46: ...rrosion and condition 4 Inspect circuit breakers for condition and security of installation APPLY EXTERNAL POWER CABIN COCKPIT 1 Check annunciator lights for operation 2 Check cockpit lighting for ope...

Page 47: ...must be clean and dry 5 Aileron bellcrank cable ends pivot bearing and control rod ends 6 Aileron and ailerontrim tab hinges and control rod ends JACK AIRCRAFT MAIN LANDING GEAR O 1 Outboard gear doo...

Page 48: ...wing WINGS 1 Flap tracks With aircraft and instrument grease MIL G 23827 lubricate the following MAIN LANDING GEAR O 1 Gear side brace link bushings and housing bushings 2 Gear torque link fittings NO...

Page 49: ...ks and security located on engine accessory case 4 Inspect oil lines and fillings for leaks security chafing dents and cracks 5 Clean and inspect oil radiator cooling fins 6 Remove and inspect oil fil...

Page 50: ...e transmitter for security and wiring Pratt and Whitney Maintenance Manual 28 Check fire extinguisher pressure If installed 29 Inspect breather tube for obstruction and security Pratt and Whitney Main...

Page 51: ...erating conditions 14 Inspect breather tube for obstructions and security 15 Inspect propeller shaft for oil leaks 16 Inspect all engine fire seals 17 Inspect engine rubber mount bushings for deterior...

Page 52: ...brokenlensesandoperation replacebulbor flashtube as required 21 Inspectwinglockerforconditionandforsecurityandoperationof hingesandlatches 22 Lubricate 23 Reinstallinspectionplatesandpanels seeCAUTION...

Page 53: ...ition and cleanliness 3 Inspect all windows for condition security and cleanliness 4 Inspect antennas for security 5 Inspect entrance and cargo doors for damage operation and security Inspect latches...

Page 54: ...ICATION Using MIL L 7870 General Purpose Low Temperature Lubricating oil lubricate the following LEFT WING 1 Nacelle locker latch rod and hinges 2 Flap transmission pivot bolts and sender arm 3 Flap t...

Page 55: ...urpose Slip Spray DuPont No 6611 lubricate the following WINGS O 1 Flap tracks With aircraft and instrument grease MIL G 23827 lubricate the following MAIN LANDING GEAR 1 Gear side brace link bushings...

Page 56: ...and fittings for leaks security chafing dents and cracks 5 Clean and inspect oil radiator cooling fins 6 Clean exterior of engine Pratt and Whitney Maintenance Manual 7 Inspect condition of ignition p...

Page 57: ...n of starter generator refer to Special Inspection 300 hour 35 Inspect tachometer generators security and wiring 36 Lubricate as per Pratt and Whitney Maintenance Manual 37 Install engine cowling RIGH...

Page 58: ...glassto checkthread endof bearingforcracksanddamage Replacebearingifball is frozenor hardto move 6 Inspectaileronbalanceweightandarm forsecurityandcondition locatedoutboardof aileron 7 Inspectflaps ac...

Page 59: ...or rod assemblies and rod end bearing assemblies for damage binding corrosion remove boot freedom of movement operation and lubrication 16 Inspect gear doors and attachments for security 17 Check warn...

Page 60: ...ove wheel clean inspect and repack bearings 6 Inspect wheel for cracks corrosion and broken bolts 7 Check tire pressure 8 Inspect shimmy dampener operation 9 Inspect gear fork for damage 10 Inspect ol...

Page 61: ...Inspectelevatortrim mechanismconditionandoperation 17 Inspectrudder elevatorcablesand trimcables for correcttensionandcondition turnbuckles guides and pulleysfor safeties damageandoperation 18 Inspect...

Page 62: ...r door actuator retraction rod end and cylinder rod end 3 Uplock hook and uplock rod 4 Door hinges 5 Upper and lower torque link connecting bolt and shimmy dampener 6 Uplockbushing 7 Forward baggage d...

Page 63: ...case 4 Inspect oil lines and fittings for leaks security chafing dents and cracks 5 Clean and inspect oil radiator cooling fins 6 Clean exterior of engine Pratt and Whitney Maintenance Manual 7 Inspec...

Page 64: ...r cracks and stress O 31 Inspect firewall seals O 32 Inspect fire extinguisher bottle pressure O 33 Inspect condition of starter generator refer to Special Inspection 300 hour O 34 Inspect tachometer...

Page 65: ...2 Inspect aileron hinges for security of attachment and operation 3 Inspect aileron balance weight and arm for security and condition 4 Inspect flap and attachment for damage and operation 5 Remove d...

Page 66: ...d strut with clean cloth soaked in hydraulic fluid MIL H 5606 FUSELAGE FORWARD DETAILED See Chapter 53 Maintenance Manual 1 Remove inspection plates and panels 2 Inspect baggage door latch hinges door...

Page 67: ...d autopilot manual 12 Inspect cabin door for damage condition of door seal and proper rig and operation 13 Replaceinspectionplates panelsandfloorpanels COCKPIT ROUTINE 1 Check pilot seat for operation...

Page 68: ...if installed 4 Pilot door latch and hinges COCKPIT 1 Control wheel rollers link and flexible joint 2 Rudder pedals torque tube bearings and blocks control cable ends and brake cylinder ends 3 Fuel pa...

Page 69: ...a battery overtemperature indication by the annunciator panel light and verified by an ammeter rise a special inspection should be performed in accordance withT 1040 Maintenance Manual Chapter 24 EMER...

Page 70: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL Page 5 41 Issued March 26 1982...

Page 71: ...DITIONER 1 Inspectair conditioningcomponentsandquillshaftsplintwearandlubricateperLubricationChart FUEL FLOW NOZZLES 1 Inspect per Pratt and Whitney Maintenance Manual 500 HOUR HEATER INSPECTION 1 Ope...

Page 72: ...for 7 1 2 centistoke or 1200 hours for a 5 centistoke oil or 9 months whichever occurs first Extensions beyond the basic drain period may be contemplated provided that the condition of the oil is mon...

Page 73: ...pter32of MaintenanceManual 2 Check emergencygear extension blow down system for operation and leaks refer to Chapter 32 of MaintenanceManual UPPER ENGINE MOUNT 1 Inspect every event and replace on con...

Page 74: ...1 Replace elevator down spring P N 51484 3000 HOUR NOTE Refer to latest Hartzell Service Letter No 61 PROPELLERS 1 Bench check or replace as required 3500 HOUR I ENGINES 1 Refer to latest Pratt and Wh...

Page 75: ...ignment check to clarify any doubt of damage MAIN LANDING GEAR EXTENSION IN EXCESS OF VLO MAX LANDING GEAR OPERATING SPEED Refer to Piper Service Bulletin 841 SEVERE TURBULENCE INSPECTION The same ite...

Page 76: ...ked ENGINE START When APU is used turn battery master switch off and monitor airplane voltmeter until reading stabilizes 27V min 30V max then turn the battery master switch on Generator switches are t...

Page 77: ...5 Cabin comfort 6 Flight controls 7 Flaps 8 Pneumatic boots check a Pneumatic pressure b Deicer switch 9 Power levers 10 Hydraulic topping governor HTG test a Propeller control b HTG test switches Set...

Page 78: ...0 RPM Np ON ON OFF CAUTION Engine Inlet Lip Deicers can be damaged if heated without the cooling effect of propeller slipstream Do not press ground test button at lower than 1800 RPM Np Perform system...

Page 79: ...R REGISTRATIONNUMBER ENGINESERIALNO PROPELLER SERIAL NO Left Left Right Right OPERATIONAL INSPECTION cont d Secondary low pitch switch CAUTION Do not release secondary low pitch stop switches with mor...

Page 80: ...CHECK LIST ENGINE FIRE GROUND Affected Engine 1 Condition lever St 2 Emergency fuel shutoff valve 3 Starter switch 4 Fuel pump 5 Ignition switch op ff n ff ff NOTE Do not attempt to restart if engine...

Page 81: ...Publications 2 Work order column is applicable only to FAA approved repair stations 3 Always check and use only current information 4 The signatures signify that this aircraft has been thoroughly ins...

Page 82: ...1 2900 2 3000 3 3100 4 3200 1 3300 2 3400 3 3500 4 3600 1 3700 2 3800 3 3900 4 4000 1 4100 2 4200 3 4300 4 4400 1 4500 2 4600 3 4700 4 4800 1 4900 2 5000 3 5100 4 5200 1 5300 2 6400 3 5500 4 5600 1 57...

Page 83: ...ROPERLY DISPLAYED 4 AIRWORTHINESS CERTIFICATE IN AIRCRAFT AND PROPERLY DISPLAYED 5 RADIO STATIONF C C LICENSES IN AIRCRAFT AND PROPERLY DISPLAYED 6 AIRCRAFT EQUIPMENT LIST WEIGHT AND BALANCE FAA FORM...

Page 84: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL w Revised March 5 1984...

Page 85: ......

Page 86: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL...

Page 87: ......

Page 88: ...MAINTENANCE MANUAL 5 21 19 Page 5 59 Revised March 5 1984...

Page 89: ......

Page 90: ...DOOR 16 RADIOS ELECTRICAL SHELF 17 AUXILIARY POWERRECEPTACLE 18 FWDOXYGENRECHARGE VALVE IFINSTALLED 19 ELECTRICAL LEADLINES 20 NOSEGEARDOORS 21 PULLEY AND CABLEINSPECTION 22 HYDRAULIC UNES ELECTRICAL...

Page 91: ...10 AILERONBELLCRANK 11 DELETED 12 AILERONCABLEANDFUEL LINE 13 AILERONCONTROL CABLE 14 FLAPTRANSMISSION 15 DELETED 16 PNEUMATICLINES 17 FLAPLIMITSWITCHES 18 LANDINGGEARDOOR 19 CABLES ANDWIRES 20 FLAPCA...

Page 92: ...1 FUELFILTER 2 HEATEXCHANGER AND PLUMBING 3 OILFILLERQUANTITY DIPSTICK 4 OILCOOLERDOORTRANSMISSION RIGHTNACELLE ONLY AIR CONDITIONING CONDENSER AND FAN 5 FUELSENDER 6 FUELFILLER CAP 7 JET PUMP 8 BLEED...

Page 93: ...CABLES 13 CONTROLCABLES PULLEYS AND TURNBUCKLES 14 CONTROL CABLES PULLEYS AND TURNBUCKLES ENGINE CONTROLLINES WIRES AND CABLES 15 HYDRAULICHAND PUMP PNEUMATIC BLOWDOWN 16 CONTROL CABLES AND PULLEYS 17...

Page 94: ...igh salt or humidity environment 3 Operation from soft or unusual terrain 4 Operation inextreme cold 5 Aircraft lightning strike 6 Engine overspeed overtorque or sudden stoppage 7 Severe turbulence ha...

Page 95: ...PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL THIS PAGE INTENTIONALLY LEFT BLANK 1D23...

Page 96: ...PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL THIS PAGE INTENTIONALLY LEFT BLANK 1D24...

Page 97: ...CHAPTER DIMENSIONS AND AREAS lEl...

Page 98: ...AS TABLEOF CONTENTS EFFECTIVITY CHAPTER SECTION SUBJECT SUBJECT 6 00 00 6 00 01 6 00 02 6 00 03 GENERAL Dimensions and Areas Station Reference Lines Access and Inspection Provisions GRID NO EFFECTIVIT...

Page 99: ...6 1 and listed in Chart 601 The serial number plate for the airplaneis locatednear the tail skid The MAA plate is locatedunderthe lower front cornerof the entrance door The engine data plates are loca...

Page 100: ...NOTE...

Page 101: ...No 12001 Latest Revision 2 3 U S Gallons 8 74 Liters Hartzell Constant Speed Feathering and Reversing HC B3TN 3B T10173K 8 93 Inches Woodward P N 8210 030 Total System Capacity Unusable Fuel 300 U S...

Page 102: ...n Tire Pressure Nose Tire Pressure Main Cleveland 40 167 or 40 167A Cleveland 30 142 18 x 4 4 6 ply Type VII Tubeless 17 5 x 6 25 6 10 ply Tube Type 6 50 x 10 10 ply Tube or Tubeless Type 90 P S I 80...

Page 103: ...ION PROVISIONS Refer to Figure 6 3 The access and inspection provisions for the airplane are shown in Figure 6 3 The components to be serviced or inspected through each opening are identified in the i...

Page 104: ...PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL FRONT SPAR ATTACH FACE REAR SPARATTACH FACE FUSELAGE Figure6 2 StationReferences 1E8 6 00 03 Page6 06 Issued March 26 1982...

Page 105: ......

Page 106: ...PIPERAIRCRAFT T 1040 MAINTENANCE MANUAL HORIZONTALSTABILIZER 104 50...

Page 107: ...T 1040 MAINTENANCEMANUAL STA STA STA Figure 6 2 Station References cont lEll 6 00 03 Page 6 09 Issued March 26 1982...

Page 108: ...TROL HORN 30 C 13 ELEVATOR TORQUE TUBE 31 S 14 NOSE CONE LATCH RELEASEACCESS 32 C 15 NOSE BAGGAGE DOOR 33 C 16 RADIOS ELECTRICALSHELF 34 C 12 UXILIARY POWER RECEPTACLE WD OXYGENRECHARGEVALVE IF INSTAL...

Page 109: ...ERON CABLE AND FUEL UNE 13 AILERON CONTROLCABLE 14 FLAP TRANSMISSION 15 DELETED 16 PNEUMATIC LINES 17 FLAP LIMIT SWITCHES 18 LANDING GEAR DOOR 19 CABLES AND WIRES 20 FLAP CABLE AILERON CONTROL CABLE E...

Page 110: ...LLE ONLY AIRCONDITIONING CONDENSER ANDFAN 5 FUELSENDER PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL LEFT NACELLE OUTBOARD LEFT NACELLE INBOARD 7 8 11 9 2 7 RIGHT NACELLE INBOARD 6 FUELFILLER CAP 7 JETPUMP...

Page 111: ...D TRIM CABLES 13 CONTROL CABLES PULLEYS AND TURNBUCKLES 14 CONTROL CABLES PULLEYS AND TURNBUCKLES ENGINE CONTROLLINES WIRES AND CABLES 15 HYDRAULIC HAND PUMP PNEUMATICBLOWDOWN 16 CONTROLCABLES AND PUL...

Page 112: ...PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL THIS PAGE INTENTIONALLY LEFT BLANK 1E16...

Page 113: ...CHAPTER LIFTINGAND SHORING E17...

Page 114: ...MAINTENANCEMANUAL CHAPTER 7 LIFTING AND SHORING TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO SUBJECT EFFECTIVITY 7 00 00 7 10 00 GENERAL 1E19 JACKING 1E19 8 82 1E18 7 ContEffec Page 1...

Page 115: ...follows 1 Placethejacks 3toncapacityor greater underthejack pads 2 Attach the tail support to the tail skid Place a minimum of 500 pounds of ballast on the support to hold the tail down CAUTION Be su...

Page 116: ...CHAPTER LEVELINGAND WEIGHING 1E20...

Page 117: ...FFECTIVITY CHAPTER SECTION SUBJECT GRID NO SUBJECT EFFECTIVITY 8 00 00 8 10 00 8 20 00 8 20 01 8 20 02 8 20 03 GENERAL LEVELING WEIGHT AND BALANCE DATA Weighing Preparation for Weighing Weighing the A...

Page 118: ...d 1 To longitudinally level the airplane partially withdraw the two leveling screws located on the right side of the fuselage nose section at station 25 60 and 57 00 Place a spirit level on these scre...

Page 119: ...weighed with full fuel tanks but it is not recommended and care must be taken to verify all fuel tanks are exactly full and not partially under or over full fuel topped off to bottom of filler neck w...

Page 120: ...he scales 3 Chock forward and aft sides of all three wheels WARNING If wheels are not blocked the airplane could roll off scales and cause serious injury and damage 4 Release emergency brake 5 If the...

Page 121: ...CHAPTER TOWINGAND TAXIING 1F1...

Page 122: ...ENANCEMANUAL CHAPTER 9 TOWING AND TAXIING TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO SUBJECT EFFECTIVITY 9 00 00 9 10 00 9 20 00 GENERAL 1F3 TOWING IF4 TAXIING 1F4 1F2 9 Cont Effec...

Page 123: ...talled In the event towing lines are necessary lines rope will be attached to both main gear struts just below the side brace link attachments Ascertain that oil cooler doors are closed Lines should b...

Page 124: ...WHEEL BASE NOSEWHEEL TRAVEL TURNING RADIUS WING TIP T 1040 WITHOUT TIPTANKS 10 FT 8 IN 40 L 40 R 29 5 FT T 1040 WITH TIP TANKS 10 FT 8 IN 40 L 40 R 29 FT 9 125 IN I Figure 9 1 Turning Radius and Limi...

Page 125: ...CHAPTER PARKINGAND MOORING lF5...

Page 126: ...CEMANUAL CHAPTER 10 PARKING AND MOORING TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO SUBJECT EFFECTIVITY 10 00 00 10 10 00 10 20 00 GENERAL 1F7 PARKING IF7 MOORING 1F7 1F6 10 Cont Eff...

Page 127: ...o block the wheels rather than setting the brakes 3 Secure the control wheel with the seat belt MOORING The airplane is moored to insure its immovability protection and security under various weather...

Page 128: ...CHAPTER REQUIREDPLACARDS 1F8...

Page 129: ...T T 1040 MAINTENANCEMANUAL CHAPTER 11 REQUIRED PLACARDS TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO SUBJECT EFFECTIVITY PLACARDS AND MARKINGS GENERAL IF10 IF10 2R 7 84 1F9 11 Cont Ef...

Page 130: ...I PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL GENERAL PLACARDS AND MARKINGS EXTERNAL Figure 11 1 Placards and Decals 1F10 11 20 00 Page 11 01 Revised July 13 1984...

Page 131: ...ACARD PROPELLER CONTROL 35 PLACARD START CONTROL 36 PLACARD POWER LEVERCONTROL 37 PLACARD ELEVATORTRIM 38 PLACARD RUDDER TRIM 39 PLACARD AILERON TRIM 40 PLACARD CIGAR LIGHTER 41 PLACARD WINDSHIELD WIP...

Page 132: ...PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL THIS PAGE INTENTIONALLY LEFT BLANK 1F12...

Page 133: ...CHAPTER SERVICING 1F13...

Page 134: ...23 04 Inflating Oleo Struts 1F20 12 23 05 Tires 1F21 12 23 06 Tire Balancing 1F21 12 24 00 Hydraulic System 1F21 12 24 01 Filling Hydraulic System Reservoir 1F22 12 25 00 Propellers 1F22 12 26 00 Eng...

Page 135: ...ECT GRID NO SUBJECT EFFECTIVITY 12 30 00 12 31 00 12 32 00 12 32 01 12 32 02 12 33 00 UNSCHEDULED SERVICING Servicing Air Conditioning System Oxygen System Oxygen System Safety Precautions Filling Oxy...

Page 136: ...ed in the bottom of each filter bowl inthe system crossfeed line and the inboard end of each fuel cell 1 To flush either filter bowl push up on the arms of the drain valve for a few seconds then repea...

Page 137: ...ITIONER 12 HOSE ENGINEOILDRAIN RIGHT AND LEFT 13 FILTER ELEMENT ENGINEOIL RIGHTANDLEFT 14 GAUGEOXYGEN PRESSURE 15 AIRCONDITIONER RECEIVER DEHYDRATOR 16 HEATER 17 FILLER OLEOSHOCKSTRUT NOSE 18 BATTERY...

Page 138: ...g procedure 1 Gain access to the brake reservoir scupper open the nose baggage door remove the tow bar and screened radio access panel 2 Clean surface around scupper and adjacent aircraft skin with a...

Page 139: ...full fuel and oil If a strut has less than the required inches exposed determine whether it needs air or oil by rocking the airplane If the airplane settles to its normal position within one cycle af...

Page 140: ...end of the tube in a container of hydraulic fluid as specified NOTE An air tight connection is necessary between the plastic tube and valve stem Without such a connection a small amount of air will be...

Page 141: ...nter of the tire Rotate the tire 450 and release it again If the tire returns to the same position add a 1 ounce patch and again rotate the tire and release it Continue this procedure until the tire i...

Page 142: ...mage and grease leakage For further information on propeller servicing refer to Chapter 61 ENGINE LUBRICATION The engine oil level should be checked within ten minutes after engine shutdown If the eng...

Page 143: ...INE OIL 1 Place suitable containers or drip pan under engine 2 Remove oil drain plug located at 6 o clock position on rear face of accessory gearbox housing and discard preformed packing 3 Remove cott...

Page 144: ...case insert the lock pin and secure with cotterpin Install chip detector on front case of reduction gearbox and torque 45 to 55 inch pounds 5 Refill the engine oil tank 6 Start the engine and run at...

Page 145: ...be replacedevery20 minutes 6 Usingclean lint freeglovesremovetheelementfromthe tankandremovetheplugs 7 Placethe elementin acleanlocationandallowto dry 8 Afterthe elementhas beencleaned inspectthe elem...

Page 146: ...hip detector by wiping with a lint free cloth and reinstall 2 If more than 10 pieces of small nugget shaped magnetic material is evident on the detector the engine should be shipped to an overhaul fac...

Page 147: ...ce of cleanliness will insure the maximum efficiency and utmost service of all moving parts Lubrication instruction regarding the locations time intervals and type of lubricants used may be found in L...

Page 148: ...cturer additional protection for the prevention of corrosion is unnecessary LUBRICATION CHARTS The lubrication charts consist of individual illustrations for the various aircraft systems and each com...

Page 149: ...2 SEE CAUTIONSNUMBER1 5 PROPELLER REMOVEONE OF THE TWOGREASEFITTINGSFOREACHBLADE APPLYGREASETHROUGH FITTINGUNTILFRESHGREASEAPPEARSAT HOLEOFREMOVED FITTING 6 LUBRICATION POINTS WIPEALL LUBRICATION POIN...

Page 150: ...GAND HOUSING BUSHING RIGHTANDLEFT 7 GEARUPLOCKHOOK CONTROLRODENDS CYLINDER ENDS RIGHT AND LEFT 8 GEAR DOOR INBOARD HINGESAND CYLINDER ENDS RIGHTAND LEFT 9 BRAKEAND POWERPACKRESERVOIR SEESPECIAL INSTRU...

Page 151: ...D NOTE2 8 UPPER ANDLOWER TORQUE LINK 9 UPPER ANDLOWERTORQUE LINKCONNECTING BOLTAND SHIMMYDAMPENER 10 GEARHOUSING BUSHINGS 11 RETRACTION RODEND 12 UPLOCK RODASSEMBLY STDANDEMER SEE SPECIAL INSTRUCTION...

Page 152: ...SAND SENDERARM 8 DELETED 9 FLAPTRACK RIGHTAND LEFT 10 FLAPTRACKROLLERS RIGHT AND LEFT 11 AILERONBELLCRANK CABLEENDS PIVOT BEARINGANDCONTROL ROD ENDS RIGHTANDLEFT 12 TRIMSCREWS 13 FLAPTRANSMISSIONSCREW...

Page 153: ...ENDSANDPULLEYS 5 ELEVATOR BELLCRANK PIVOTBOLTSAND CABLEENDS 6 RUDDER HORNCABLEENDS 7 ELEVATOR TRIMSCREW SEESPECIAL INSTRUCTION 3 8 ELEVATOR TRIMTAB CONTROL RODENDS 9 ELEVATOR CONTROL ROD LUBRICANT MIL...

Page 154: ...L RODENDS 5 OILFILTERELEMENT LUBRICANT MIL G 23827 MIL G 23827 LUBRIPLATE 130A MIL G 23827 FREQUENCY 100 HRS 100 HRS 100 HRS 100 HRS REFER TO SPECIALIN STRUCTION NO 1 REFER TO SPECIAL IN STRUCTION NO...

Page 155: ...0 HRS 100 HRS 100 HRS 100 HRS MIL G 21164C 500 HRS MIL G 23827 MIL L 7870 MIL L 7870 500 HRS 100 HRS 100 HRS NOTE FILL TRANSMISSION GEAR BOX 75 MINIMUM FULL WITH DUKE P N 2196 74 1 LUBRICANT SKETCH A...

Page 156: ...UENCY MIL L 7870 MIL L 7870 MIL L 7870 MIL L 7870 100 HRS 100 HRS 100 HRS 100 HRS Figure 12 9 Lubrication Chart Cabin Door Baggage Door and Seats COMPONENT 1 SPUNESOFQUILLSHAFT LUBRICANT MIL G 21164 P...

Page 157: ...s up to eleven outlets The oxygen cylinder may be either forward or aft mounted Maintenance instructions for the oxygen system may be found in Chapter 35 OXYGEN SYSTEM SAFETY PRECAUTIONS The utmost ca...

Page 158: ...owest pressure When found if this cylinder has a pressure lower than the oxygen cylinder in the aircraft do not attempt using it for filling use the storage cylinder that has a pressure higher than th...

Page 159: ...Try not to direct any water pressure at these seals Water couldfreeze and bind cables under certain conditions 1 Allow the engine to cool for at least 40 minutes before performing a compressor wash 2...

Page 160: ...e to chemicals in tap water which may cause deposits on compressor blades tap water should not be used CAUTION Observe starter operating limits of 30 seconds on 60 seconds off 30 seconds on 60 seconds...

Page 161: ...PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL 1G17 THRU 1G20 INTENTIONALLY LEFT BLANK 1G17...

Page 162: ...CHAPTER STANDARDPRACTICES AIRFRAME IG21...

Page 163: ...1 Headliner Side Panels and Seats 1H8 20 22 02 Carpets 1H8 20 23 00 Cleaning Exterior Surfaces 1H8 20 23 01 Windshield and Windows 1H8 20 23 02 Landing Gear 1H9 20 23 03 Field Cleaning Engine 1H9 20 2...

Page 164: ...15 20 25 16 20 25 17 20 25 18 20 26 00 20 27 00 AIRCRAFT FINISH CARE cont Difficulties with Polyurethane Application of Polyurethane Difficulties with Acrylics Application of Acrylics Trim and Regist...

Page 165: ...the way they are supported during a tightening operation Any instructions furnished by the manufacturer must be followed explicitly When it is necessary to use a special extension or adapter wrench t...

Page 166: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL C Figure 20 1 Torque Wrench Extension HERE 20 10 01 Page 20 02 Issued March 26 1982...

Page 167: ...y damage the sheets It is recommended that a small center drill be used to provide a guide for a larger drill on top of the rivet stem and the tapered portion of the stem be drilled away to destroy th...

Page 168: ...lareless tube fittings eliminates all tube flaring another operation referred to as presetting is necessary prior to installation of a new flareless tube assembly which is performed as follows 1 Cut t...

Page 169: ...BROWN REDNUMERALS AND LETTERS D FLAME AROMATIC AND OIL RESISTANT HOSE HOSEIDENTIFICATION ORANGE ORANGE ORANGE GRAY ELECTRICAL COMPRESSED INSTRUMENT CONDUIT GAS AIR GREEN RED ORANGE BLUE BREATHING FUEL...

Page 170: ...CONE SLEEVE PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL TUBING SYSTEM LUBRICANT HYDRAULIC FUEL OIL SLEEVE SLEEVE PI Page 20 06 Issued March 26 1982...

Page 171: ...Gasoline and Oil Resistant Oxygen Ribbon DopeThread Sealant Permacel 412 Pitot and Static TT A 580 JAN A 669 Anti Seize Compound White Lead Base NOTE Lubricate engine fittings only with the fluid con...

Page 172: ...se a mild soap and water solution Loose dirt should be flushed away with clean water Harsh abrasive or alkaline soaps or detergents could cause corrosion or make scratches in the finish Use naphtha an...

Page 173: ...solution with a rag sponge or soft bristle brush 3 To remove stubborn oil and grease use a cloth dampened with naphtha 4 Where exhaust stains exist allow solution to remain on the surface longer A cl...

Page 174: ...ing the landing gear place a plastic cover or similar material over the wheel and brake assembly 1 Place a pan under the gear to catch waste 2 Spray or brush the gear area with solvent or a mixture of...

Page 175: ...lating is necessary between two contacting dissimilar surfaces 2 3 coats of zinc chromate or a coat of epoxy polyamid on each surface plus a 003 thick piece of vinyl tape if one of the surfaces is mag...

Page 176: ...he exterior skins wheel and wheel well areas battery compartment fuel cell and all other drains and any bilge areas not requiring extensive removal of inspection access covers B Detailed inspection sh...

Page 177: ...ans Aluminum White to grey powdery material Mechanical polishing or brushing with material softer than aluminum Magnesium highly susceptible White powdery snow like to corrosion mounds and white spots...

Page 178: ...slots and equipment installed in these areas may corrode unnoticed unless a careful surveillance is maintained 7 Engine frontal areas air inlet ducts and the leading edge of wings because they are con...

Page 179: ...whatever is handy Almost any kind of cover will either smother the fire or a least contain it until a fire extinguisher can be brought to the can Another safety factor is the importance of proper air...

Page 180: ...Cleaning General A large majority of paint strippers metal brighteners and solvents will either attack the exposed sealant the anti static coatings on the glass or the exposed plastic Contact with th...

Page 181: ...uction cup gun may vary from 20 55 PSI SPRAY PATTERNS Be sure the paint is thinned sufficiently Do not exceed paint manufacturer s specifications The use of a Zahn cup and stop watch is recommended to...

Page 182: ...until the thinner appears clear NOTE Remove pressure from equipment before beginning cleanup Then soak only the nozzle in thinner to further clean the head Lubricate the air valve stem and all the pa...

Page 183: ...gives the thickest coat along the edge and blends out in the flat portion Figure 20 9 A single layer of material laid on the surface by one pass of the gun will be typically about 10 to 12 inches wide...

Page 184: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL PROPER IMPROPER Figure 20 8 Spray Technique Figure 20 9 Spraying Corners 1H19 20 25 06 Page 20 20 Issued March 26 1982...

Page 185: ...the fuselage and spanwise on the vertical and horizontal tail surfaces and the wing After the primer has cured for the proper time and is ready to receive the top coats the same sequence is used to s...

Page 186: ...t has been loosened from the bottom 4 After being certain that every bit of the pigment is in suspension box the material by pouring it back and forth between the two containers until it is THOROUGHLY...

Page 187: ...g this second coat will probably run or sag The same will happen if the paint is applied to a cold skin when the air is warm The pressure pot should have a slow moving agitator to keep the pigments fr...

Page 188: ...metallic colors use 65 PSI Apply a light medium tack coat Allow to set up for 20 minutes Repeat for a second coat Then reduce 15 with 8485S 17 18 seconds in a 2 Zahn cup and apply a third light mediu...

Page 189: ...hours NOTE Use primer within 6 hours of mixing Discard any remaining mixture E Mix Ranthane color according to manufacturer s directions and apply within 48 hours of priming Spray one very thin mist c...

Page 190: ...ering is encountered during application anti crater solution may be added to the primer solution not to exceed one ounce per gallon of catalyzed thinned primer solution Allow catalyzed primer to stand...

Page 191: ...lyst 1 2 part enamel reducer except when using flat black then increase enamel reducer to 2 parts and 4 parts urethane enamel Allow to stand for 15 minutes then remix before use Thin as required with...

Page 192: ...ive air pressure must be used If the acrylic film is sprayed on too thick it may produce a glassy surface but it may appear hazy if viewed from the side instead of directly This is due to tiny air bub...

Page 193: ...ries When the top of the fuselage is to be painted white with a dark color adjoining it apply the light color and feather it into the area to be painted with the dark color When the light color has dr...

Page 194: ...er fresh successive coatings of wash primer and modified zinc chromate They will also adhere to freshly applied epoxy coatings dried less than 6 hrs 5 Epoxy topcoats will adhere to all paint systems t...

Page 195: ...ll not have as much of an opportunity to pack at the bottom of the can Empty containers should be disposed of properly Because the useful life of some finishes is limited use the older materials first...

Page 196: ...pened with dry cleaning solvent 3 Metal Decals A Cellophane Backed 1 Immerse in water for 1 3 minutes 2 Remove and dry 3 Remove cellophane backing 4 Position on receiving surface For large foil decals...

Page 197: ...llow Pan or Tray Squeegee and Sponge DESCRIPTIONS Meyercord 1505 gly Meyercord 1647 Meyercord 1698 S SUPPLIERS Meyercord Corporation 365 East North Avenue Carol Stream Wheaton Illinois 60187 Phone 312...

Page 198: ...PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL GRIDS 119THRU 1L24 INTENTIONALLY LEFT BLANK 119...

Page 199: ...MAINTENANCE MANUAL CARD 2 OF5 PA 31T3 T1040 PIPER AIRCRAFT CORPORATIO PART NUMBER 761765 2A1...

Page 200: ...broken down into Sub System Sections These sections are identifiedby thesecondelement ofthe standardized numberingsystem Thenumber 40 of thebasicnumber series 32 40 00is for the Wheelsand Brakes porti...

Page 201: ...complete list of Charts is for all fiche in this set followinglist of Illustrations 4 A completelist of paragraph titlesandappropriate Grid locationnumbersisgivenat the beginningof each Chapter relat...

Page 202: ...5 1 2 3 4 and 5 1 2 3 4 and 5 1 2 3 4 and 5 1 2 3 4 and 5 3 2 INTERIM REVISION Revisions appear in Chapter 27 of card 2 Please dispose of your current card 2 and replace it with the revised card DO N...

Page 203: ...al P N DC 3176 5A Marathon Nickel Cadmium Battery Instruction Manual P N BA 89 DE ICE SYSTEM PROPELLERS B F Goodrich Electrothermal Propeller Deice Maintenance Manual P N 68 04 712 Latest Revision B F...

Page 204: ...nual All Models Lear Siegler Inc Overhaul Manual Series 23048 P N 8013C P N 23700 P N 23202 PIPER PUBLICATIONS PARTS CATALOG INSPECTION 761761 Piper Aircraft Corporation 820 E Bald Eagle Street Lock H...

Page 205: ...0497 Air Conditioning System Electronic Leak Detector Autopilot Avionics TIF Instruments 3661 N W 74th Street Miami Florida 33147 305 696 7100 Edo Corporation Avionics Division P O Box 610 Municipal...

Page 206: ...gines The B F Goodrich Company 6400 Goldsboro Road Suite 102 Bethesda Maryland 20034 301 229 5000 Leach Corporation 5915 Avalon Boulevard Los Angeles California 90003 213 232 8221 Narco Avionics Inc 2...

Page 207: ...General Controls 801 Allen Avenue Glendale California 91201 213 842 6131 Aeroquip Corporation Marmon Division 1214 Exposition Boulevard Los Angeles California 90064 213 774 3230 Aerosonic Corporation...

Page 208: ...tor Woodward Governor Company Drake and Lemay Roads Fort Collins Colorado 80521 303 482 5811 Auxilec Incorporated One Willow Park Center Farmingdale New York 11735 516 694 1441 Lear Siegler Incorporat...

Page 209: ...NG AND TAXIING PARKING AND MOORING REQUIRED PLACARDS SERVICING STANDARD PRACTICES AIRFRAME ENVIRONMENTAL SYSTEM AUTOFLIGHT COMMUNICATIONS ELECTRICAL POWER EQUIPMENT FURNISHINGS FIRE PROTECTION FLIGHT...

Page 210: ...STRUCTURES DOORS FUSELAGE STABILIZERS WINDOWS WINGS PROPELLER STANDARD PRACTICES ENGINES POWER PLANT ENGINE TURBO PROP ENGINE FUEL SYSTEM IGNITION AIR ENGINE CONTROLS ENGINE INDICATING OIL SYSTEM STAR...

Page 211: ...r Doors 1G11 12 9 Lubrication Chart Cabin Door Baggage Door Seats 1G12 12 10 Lubrication Chart Air Conditioner Quill Shaft 1G12 20 1 Torque Wrench Extension 1HI 20 2 Correct Method of Installing Rod E...

Page 212: ...Installing Pulley and Drive Plate Bearing 2E8 21 35 Installing Pulley and Drive Plate 2E8 21 36 Removing Coil Housing Retaining Ring 2E9 21 36a Positioning Sankyo Compressor Internal Parts 2E11 21 36b...

Page 213: ...ion of Aileron Rigging Tool 2J13 27 9a Wrapping Control Pedestal Aileron Trim Drum 2J 16 27 10 Trim Controls Installation 2J17 27 11 Aileron Control Travels and Cable Tension 2J 18 27 12 Safety Wiring...

Page 214: ...Pump 3C10 28 15 Test Equipment Hookup 3C15 28 16 Alternate Indicator Bench Test Hookup 3C18 28 17 Fuel Gauge Adjustment 3C19 29 1 Schematic Diagram Hydraulic System 3D20 29 2 Schematic of Power Pack...

Page 215: ...se of Dial Indicator 3H17 30 20 Centering of Brushes on Slip Rings 3H 18 30 21 Wiring Schematic Electric Propeller Deicing System 3H 18 30 22 Modular Brush Assembly Wear Check 3H20 30 23 Angle of Cont...

Page 216: ...itch 31 16 32 27 Gear Warning Suitches Installation 31 16 32 28 NoseGear Wear Limits 3L18 32 29 Main Gear Wear Limits 3L21 33 1 Logo Light Assembl Adjustments 4B1 7 34 1 Instrument Air System Installa...

Page 217: ...ancing 4115 61 1 Propeller Installation 4122 61 2 Typical Nicks and Removal Method 4123 61 3 Propeller Governor 4J3 61 4 Propeller Synchrophaser Installation Woodward Type 1 4J5 61 5 Propeller Synchro...

Page 218: ...rt No 18338 00 5H9 95 2 Fabricated Tail Stand 5H10 95 3 Protective Closures Installation 5H II 95 4 Fabricated Bellcrank Rigging Tool 5H 12 95 5 Fabricated Aileron and Elevator Rigging Tool 5H 13 95 6...

Page 219: ...ted 2G21 2405 Specific Gravity Temperature Correction 2G22 2406 Capacity Ratings at Discharge Rates 2G23 2407 Electrolyte Freezing Points 2G23 2408 Circuit Load Chart 2H7 2601 Pressure Temperature Cor...

Page 220: ...hooting Pneumatic System Pressure Gauge 4E5 3903 Troubleshooting Engine Oil Pressure Gauge 4E5 3904 Troubleshooting Fuel Pressure Gauge 4E6 3905 Troubleshooting Air Temperature Gauge 4E9 3906 Troubles...

Page 221: ...ibration Data 5C21 7702 Digital Analog Torque Calibration Data 5C23 7703 Weston Kulite Torque Pressure Indicating System Tansducer Voltages 5C24 7901 Oil Pressure Gauge Calibration Data 5D17 9101 List...

Page 222: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2A24...

Page 223: ...CHAPTER ENVIRONMENTAL SYSTEM 2B1...

Page 224: ...ter 2B19 21 42 03 Installation of Heater 2B20 21 42 04 Disassembly of Heater 2B20 21 42 05 Reassembly of Heater 2B23 21 42 06 Spark Plug 2C 21 42 07 Removal of Spark Plug 2C1 21 42 08 Installation of...

Page 225: ...Installation of Combustion Air Pressure Switch 2C10 21 42 33 Overheat Switch 2C10 21 42 34 Removal of Overheat Switch 2C10 21 42 35 Installation of Overheat Switch 2C11 21 42 36 Duct Switch 2C11 21 42...

Page 226: ...Maintenance 2D22 IR 3 84 21 56 01 Compressor Service 2D22 21 56 02 Delco Compressor 2D22 A 3 84 21 56 03 Compressor Removal 2D22 21 56 04 Belt Inspection Delco and Sankyo Compressor Installation 2D23...

Page 227: ...of Fan and Condenser Installation of Fan and Condenser Receiver Dehydrator Removal Receiver Dehydrator Installation Expansion Valve Removal Expansion Valve Installation Evaporator Removal Evaporator...

Page 228: ...the temperaturedrops belowa predeterminedlimit The heater OVER TEMP light can be reset and the heater restarted by using the PUSH TO RESET button An additional scoop mounted on the bottom of the airpl...

Page 229: ...t switch open Bad spark plug Apply external power supply Attempt to start heater Turn on manual shut off valve or master solenoid Remove the nozzle and clean or replace it Remove and check sole noid R...

Page 230: ...or ice in fuel system Ventilating air blower fails to run Mounted separate from combus tion heater Heater switch OFF Broken or loose wiring to motor Energize the heater switch Check and repair wiring...

Page 231: ...fuel lines Inspect fuel supply to heater including shut off valve solenoid valve fuel filter fuel pump and lines Make necessary repairs Spark plug partially fouled Replace spark plug CAUTION Do not c...

Page 232: ...n or replace the nozzle as required Heater starts then goes out Lack of fuel at heater Check fuel supply through all components from the tank to the heater Make nec essary corrections Inoperative or c...

Page 233: ...ERINSTALLATION 4 DEFROSTEROUTLET 5 FRESHAIR OUTLET COCKPIT 6 HEATERDUCT 7 FRESHAIR INLET SCOOP 8 VENTILATING BLOWER 9 VENTILATION DUCT 10 FRESHAIR OUTLET CABIN 11 HEATER DUCT 12 CABIN EXHAUST 13 GROUN...

Page 234: ...SURE SWITCH 5 COMBUSTION AIR INTAKE TUBE 6 COMBUSTION AIR BLOWER 7 VENTILATING AIR BLOWER 8 VENTILATING AIR INTAKE VALVE 9 SPARK PLUG 10 TERMINAL STRIP 11 LIMIT STRIP 12 HEATER EXHAUST PIPE 13 HOURMET...

Page 235: ...emperaturefor desiredcomfort level If this switch is set for ground operating comfort it may be necessaryto reposition it after being airborne since ram air will increasethe ventilatingair flowand the...

Page 236: ...uctions Run a wire through it ifnecessary clearan obstruction 3 Check all fuel lines for security at joints and shrouds making sure that no evidenceof leaks exists Also check for security of attachmen...

Page 237: ...tep 3testingand Figure21 4 5 Replacethe vibrator in the ignition unit only when it no longer functions CAUTION Ignition assembly will be damaged if ignition lead is arced to ground other than through...

Page 238: ...ooth and medium brown in color Replacethe motor ifthe commutator or other parts show damage 13 Inspect the combustion air blower motor as described in the preceding step 14 Inspect the blower wheel fo...

Page 239: ...itch opening with a water manometer and needlevalve in the line ahead of switch Switch must be tested in 45 degree position or as installed in the airplane B Connect an ohmmeter across the switch term...

Page 240: ...STOPPER DRILL OUT TO _ t NECESSARYDIA CLAMP SEALCAP Figure 21 3 SuggestedDesign tor Seal Plate Plugs and Caps for Combustion Tube Leakage Test 427 1 1 WATER MANOMETER 2 OHMMETER 3 NEEDLEVALVE 4 TEE 5...

Page 241: ...heater isa kerosene fuel operated 24 Vdc electrically controlled unit installed inthe nose section just forward of bulkhead Sta 57 00 REMOVAL OF HEATER 1 Turn the heater control switch off 2 Remove t...

Page 242: ...the side of the fuselage DISASSEMBLY OF HEATER Refer to Figure 21 5 1 Remove the screw and slide the elbow adapter off the combustion air inlet tube 2 Disconnect and remove electrical wiring and indiv...

Page 243: ...2 COATSCREWS AND BOTHSIDES OF GASKET WITH PERMATEX NO 1372 FORM A GASKET 3 COATSCREWS ANDBOTHSIDES OF GASKETWITH RTV NO 732 SILICONE RUBBER SEALANT 33 24 28 SEENOTE 2 3 18 30 SEENOTE1 I Figure 21 5 E...

Page 244: ...13 MACHINE SCREW 14 FLAT WASHER 15 SHELL COVER 16 O RING 17 SOLENOIDCOIL 18 BASE PLATE 19 KNURLED NUT 20 O RING 21 TERMINAL STRIP 22 INSULATOR 23 MACHINE SCREW 24 COMBUSTION AIR INLET ADAPTER 25 OVER...

Page 245: ...six screws that attach the combustion head assembly to the combustion tube and jacket assembly and lift out of combustion tube REASSEMBLY OF HEATER Refer to Figure 21 5 When reassembling the heater u...

Page 246: ...l the ignition assembly on the jacket assembly with the four screws Connect the high voltage lead to the spark plug and tighten it to 20 foot pounds 13 Attach the overheat limit switch and two spacer...

Page 247: ...trode on the plug NOTE The spark plug can be checked visually for sparking across the gap prior to installing the plug Disconnect the wire from the No 3 terminal on the heater wiring side of the termi...

Page 248: ...g under all flight conditions Heat is produced by burning a fuel air mixture in the combustion chamber of the heater Fuel is injected into the combustion chamber through the spray nozzle The resulting...

Page 249: ...CIRCUIT FILTER RESISTOR TOTAL RESISTANCE A TO B MUST NOT EXCEED 0 3 OHMS Figure 21 6 Wiring Test Setup 381 HIGH VELOCITY WHIRLING FLAME SPARK PLUG COMBUSTION AIR FUEL INLET HEATED AIR SOLENOID EXHAUS...

Page 250: ...heater jacket with the high voltage cable facing the spark plug end of the heater 2 Install the four screws and tighten the screws securely 3 Carefully connect the high voltage lead to the spark plug...

Page 251: ...e replaced only when it no longer functions REMOVAL OF VIBRATOR 1 Remove the hose type clamp from the housing brackets that secure the vibrator 2 Remove the vibrator from the ignition unit it may requ...

Page 252: ...for the first hour then gradually increase the speed until it is rotating at approximately normal speed Continue the run in operation for at least two hours to properly seat the brushes before instal...

Page 253: ...and clean all exterior surfaces thoroughly CLEANING AND INSPECTING THE COMBUSTION TUBE ASSEMBLY Refer to Figure 21 5 1 Slight scaling and discoloration of the combustion tube assembly is a normal con...

Page 254: ...nings uncovered direct a stream of compressed air into the combustion tube assembly from first one opening then the other Make sure all loose material is removed REPAIR OF COMBUSTION TUBE ASSEMBLY No...

Page 255: ...3 MOTOR COMBUSTION AIR BLOWER 13 PLATE SWITCH ACTUATOR 4 SCREW 14 MICRO SWITCH 5 BRUSH 15 BLOWER WHEEL 6 SWITCH 16 BLOWER INLET ADAPTER 7 CAPACITOR 17 DUCT SWITCH 8 BRACKET 9 SPACER 10 HOUSING Figure...

Page 256: ...ise caution not to overtorque the switch as this could change the setting 2 Connect the tube assemblies to the switch using a suitable thread lubricant 3 Connect the electrical leads to the appropriat...

Page 257: ...146 F 6 The switch has differential of 10 F 5 at any given setting An override switch has been added to the duct system switch to override the duct switch at the last portion of its travel to the hig...

Page 258: ...op Then carefully place the control lever arm on the shaft at the high position and lock the lever by tightening the allen head set screw Do not over tighten Rotate the lever arm to make sure it clear...

Page 259: ...te of these connections for correct installation 3 Disconnect the screws attaching the unit to its mounting bracket ADJUSTMENT OF FUEL REGULATOR AND SHUTOFF VALVE The fuel regulator and shutoff valve...

Page 260: ...nd other factors which would be accomplished in a laboratory type test If such a test cannot be made install the heater and check operation on the ground and in the air to determine if operation is no...

Page 261: ...d reconnect the terminal lead disconnected in preceding step 5 10 Close the power supply switch and turn on the fuel supply The heater should light within five seconds may require slightly longer for...

Page 262: ...2 6 APPROX FUEL IN FROM PUMP 2 25 DIA ORIFICE 13 14 28V 12 Figure 21 11 Suggested Setup for Heater Operation Test C614 COMBUSTION RADIO Al LOWER RADIO NOISE FILTER FILTER VENTILATING AIR SWITCH NOISE...

Page 263: ...fittings and remove the filter 6 Disassemble filter and inspect filter element for contamination then reassemble filter NOTE Inspectfilter first 100 hours of operationand then every detailed inspecti...

Page 264: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL GRIDS 2C18 THRU 2C20 INTENTIONALLY LEFT BLANK 2C18...

Page 265: ...through the condenser to the spar box and into the cabin evaporator modules The pressure and suction lines run approximately parallel The suction line is the larger of the two The air conditioner is a...

Page 266: ...ng clamped to suction on suction line line If capillary and compressor bulb OK replace suction service expansion valve valve Restriction in Check for kinked liquid line hoses and stopped from condense...

Page 267: ...frost may read a Expansion valve Remove screen vacuum in inlet screen Clean with sol dicating evap clogged vent and replace orator lacks Inoperative ex Warm capillary by refrigerant pansion valve hol...

Page 268: ...place valves with compressor valve kit valves System produces Electrical no cooling Open circuit Reset circuit breaker breaker Broken or dis Check all termi connected elec nals for loose trical wire c...

Page 269: ...r partially Remove compressor or completely for service or re frozen placement Expansion valve Replace expansion stuck in open valve position Refrigeration Broken refrigerant Examine all lines line fo...

Page 270: ...motor motor sluggish for serviceor in operation replacement Mechanical Compressor clutch Remove clutch slipping assembly for ser vice or replace ment Obstructed blower Examine entire passage passage f...

Page 271: ...Purge system replace receiver dehydrator receiver dehydrator Excessive moisture Purge system replace in system receiver dehydrator Air in system Purge evacuate and charge system Replace receiver NOTE...

Page 272: ...ce ment Compressor oil Fill with correct level low amount of speci fied oil Circulating fan Remove blower noisy excessive motor for ser wear in blower vice or replace motor ment as necessary Refrigera...

Page 273: ...PORT SERVICE VALVE SUC RTION ___ _ LOW PRESSURE SWITCH FREON SUCTION RECEIVER MAGNETIC CLUTCH VIEWA A ___ VENTILATING DUCT EVAPORATOR SIGHT GLASS FREEZE PROTECTION SWITCH EXPANSION VALVE VENTILATING...

Page 274: ...CLUTCH 5 FIREWALL FITTINGS 6 THERMAL SWITCH 7 FREONPRESSURESWITCH 8 LOW FREONPRESSURESWITCH 9 RECEIVER DEHYDRATOR 10 VENTILATING DUCT 11 BLOWER 12 EVAPORATOR 13 EXPANSION VALVE 14 FREONCONDENSER Figur...

Page 275: ...18 3 16 134 73 19 7 18 137 74 21 20 140 75 22 4 22 144 76 23 1 23 148 77 23 8 24 152 78 24 6 25 156 79 25 3 26 160 80 26 1 27 162 81 26 8 28 165 82 27 6 29 167 83 28 4 30 170 84 29 2 31 172 85 30 32...

Page 276: ...chart indicates It must be pointed out that the actual temperature of the air passing over the coils of the evaporator will be several degrees warmer allowing for a temperature rise caused by the los...

Page 277: ...ng inspection of the system PERFORMANCE TEST IN COLD CLIMATES To run a performance test on the T 1040 air conditioning in cold climate below 70 F the following procedures will have to be used 1 Obtain...

Page 278: ...Always wear safety goggles when handling refrigerant WARNING One of the most important precautions is protection of the eyes when handling refrigerant Any liquid refrigerant which may accidentallyesc...

Page 279: ...tions Refer to Chart 2104 9 To insure a consistent seal on all flared and pipe fittings used on the air conditioning system seal the fittings with Loctite refrigerant sealant Sealant should be applied...

Page 280: ...ecorded on the gauge above the hose Cracking the hand valve in the counterclockwise direction opens the systemto the middle service port of the manifold set This is desirable only when it is necessary...

Page 281: ...slight amount of refrigerant gas to escape from the Schrader valvefitting 3 The cylinder of refrigerant should be placed upright in a container of warm 125 F max water on a small scale 5 Allow approx...

Page 282: ...e the exhaust port on the vacuum pump is open to avoid damage to the vacuum pump 5 Operate the vacuum pump and open the low side manifold hand valve Observe the compound low pressure gauge needle it s...

Page 283: ...MAINTENANCE MANUAL 1287 CLOSED CLOSED L DIAGRAM A CRACKED Page 21 55 CLOSED H DIAGRAM B CRACKED CLOSED DIAGRAM C CRACKED CRACKED DIAGRAM D Figure 21 16 Manifold Set Operation 21 54 00 Page 21 55 Issu...

Page 284: ...RVICE VALVE TO VACUUM PUMP OR REFRIGERANT CYLINDER Figure 21 17 Test Gauge and Manifold Set C468 MANIFOLD PRESSURE GAGE SET COMPOUND GAGE BAGAGE 50 P S TO COMPRESSOR OPEN CLOSED REFRIGERANT CONTAINER...

Page 285: ...g LineOpen Only When Evacuating NOTE SHUT OFF VENT LINE TIGHTEN KNURLED FITTING FINGER TIGHT ONLY DO NOTOVERTIGHTEN FITTING CHARGING RESEVOIR EVACUATINGt C 1 542E CONNECTOR C468 PRESSURE MANIFOLD GAGE...

Page 286: ...o not allow refrigerant to escape too rapidly as excessive oil may be carried out of system When hissing stops pressure should read zero indicating the system is empty and service valves should be clo...

Page 287: ...at top of cylinder behind control panel intermittently to relieve pressure and allow refrigerant to continue filling cylinder D When refrigerant reaches desired level in the sight glass close both the...

Page 288: ...move charging lines from compressor using care due to the small amount of refrigerant remaining in the lines Cover Schrader fittings with a shop rag during removal of lines to catch escaping refrigera...

Page 289: ...E When no leaks are evident close service valves on compressor remove gauge set and proceed with charging per Step 4 3 EVACUATING SYSTEM USING SYSTEM COMPRESSOR NOTE This method is the least desirable...

Page 290: ...nt container valve and purge the line by opening the valve and allowing refrigerant gas to flow through the hoses Tighten the hose at the gauge set open the low pressure gauge valve C With the right e...

Page 291: ...uld not be confused with that given under Checking and Adding Oil which is for checking total oil in the air conditioning system 12 While working over a draining tray and with the clutch end up comple...

Page 292: ...ROD 2 BOTTOM MOUNTING BOLT 3 ADJUSTMENT BRACKET 4 TOP MOUNTING BOLT Figure 21 21 Compressor and Drive Assembly UNEVEN CUT INTER CROWN DELAMINATION FUZZY CORD SOFT CARBON OR BUBBLES Figure 21 22 Belt I...

Page 293: ...TE DELCO COMPRESSOR SHOWN COMPRESSOR DRIVE ADJUSTMENT ROD TOP MOUNTING BOLT DRIVEBELTS COMPRESSOR Figure 21 23 Drive Housing and Drive Assembly EFFECTIVITY 21 56 04 DELCO AND SANKYO Page 21 65 COMPRES...

Page 294: ...ension B On the initial installation of the belts adjust the tension to 100 5 pounds C After initial compressor operation of up to 1 hour recheck the tension If the recheck is made immediately after t...

Page 295: ...hour it will be necessary to warm the compressor case for 15minutes by a light source or heat gun The compressor must be slightly warmer than the rest of the air conditioning system to drive out all...

Page 296: ...TORS GUAGE SET L P H P CONTAINER OF WATER COMPRESSOR 125 F SCHRADER OVERTIGHTEN VALVES SERVICEHOSE O RING KNURLED FITTING NOTE SEE NOTE TIGHTEN KNURLED FITTING FINGER TIGHT ONLY DO NOT OVERTIGHTEN FIT...

Page 297: ...1 Figure 21 26 Removing Driven Plate 578 DRIVE PLATE DRIVENPLATE SCORING OF DRIVE AND DRIVEN PLATE IS NORMAL DO NOT REPLACE FORTHIS CONDITION Figure 21 27 Drive and Driven Plates 21 56 07 EFFECTIVITY...

Page 298: ...0 2 X Figure 21 28 Aligning Driven Plate Key Figure 21 29 Installing Driven Plate A B J 6435 RETAINING RING CLEARANCE 030 057 Figure 21 30 Checking Air Gap Figure 21 31 Removing Pulley Retaining Ring...

Page 299: ...end of the compressor with tool J 9481 Refer to Figure 21 34 The pulley should rotate freely 2 Install the pulley retaining ring with tool J 6435 3 Insert the square drive key into the shaft of the co...

Page 300: ...ive Plate Figure 21 33 Removing Bearing J 8092 J 8092 J 8092 THIS RIDGE OF TOOL UP WHEN INSTALLING BEARING J 9481 J 9481 Figure 21 34 Installing Pulley and Drive Figure 21 35 Installing Pulley and Dri...

Page 301: ...coil housing retaining ring with tool J 6435 2 Remove the clutch coil housing retaining ring with tool J 6435 3 Remove coil housing assembly INSTALLATION OF CLUTCH COIL AND HOUSING 1 With the scribe...

Page 302: ...After initial compressor operation of up to one hour recheck the tension If the recheck is made immediately after the engine is shut down hot and belt tension is below 50 lbs readjust the tension to 5...

Page 303: ...as they are moving to the front of the compressor suction stroke NOTE This step is necessary to clear the dipstick of internal parts and to allow its insertion to full depth 6 Insert the dipstick to i...

Page 304: ...30 ANGLE Figure 21 36b Fabricated Dipsticks for Compressor Oil Check MOUNTING DIPSTICK MOUNTING ANGLE RIGHT STOP ANGLE LEFT POSITION 7 TOP OIL FILLERHOLE CLUTCH FRONT PLATE Figure 21 36c Sankyo Compre...

Page 305: ...ts 0 4 6 10 6 8 20 8 10 30 10 11 40 11 12 50 12 13 60 12 13 90 15 16 C745 6 1 HEX NUT 8 2 FRONT PLATE 3 SHAFT KEY 4 SHIMS 5 SNAP RINGS 6 ROTORPULLEY 7 BEARING 8 CLIP 9 COIL 10 COMPRESSOR 11 COIL LEAD...

Page 306: ...LATION OF MAGNETIC CLUTCH PULLEY AND COIL I Install field coil Coil flange protrusion must match hole in front housing to prevent coil movement and correctly locate lead wire A Install snap ring B Pos...

Page 307: ...e shaft 8 Disconnect the bracket from the firewall and remove the fan motor and fan blades from the nacelle 9 Disconnect the hardware holding the condenser 10 Remove the condenser from the nacelle NOT...

Page 308: ...ar underneath the first passenger s seat on the right hand side 1 Discharge the system of all refrigerant 2 Disconnect the refrigerant lines at the receiver dehydrator Cap the end of the lines to prev...

Page 309: ...box 1 Remove the appropriate seat s from the airplane 2 Remove the seat tracks and carpet from the floorboard panel 3 Remove the screws securing the floorboard panel over the unit and remove the panel...

Page 310: ...securing the floorboard panel over the unit and remove the panel 5 The air conditioning system must be completely discharged before disassembly 6 Remove the inboard end panels of the modules 7 Loosen...

Page 311: ...iously removed and secure BLOWER AND MOTOR ASSEMBLY The blower and motor assemblies are located in the spar box on the outboard side of the evaporator assemblies BLOWER AND MOTOR ASSEMBLY REMOVAL 1 Re...

Page 312: ...BLOWER Figure 21 39 Sealing of Ducts B112 NOTE USE VO1 SHAN SEALS VSF1015A6BX PIPERCODE 486 476 FOR 4 DIA TUBE VSF1015A8BX PIPERCODE486 479 FOR 1 DIA TUBES VSF1015A12BX PIPERCODE 486 478 FOR3 4 DIA T...

Page 313: ...xcept tighten only once CAUTION When installing Voi Shan seals check for cracks and scored flared ends and nipple ends Replace parts as necessary 3 Leaks are most frequently found in the nacelle area...

Page 314: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL GRIDS 2E22 THRU 2E24 INTENTIONALLY LEFT BLANK 2E22...

Page 315: ...CHAPTER AUTO FLIGHT 2F1...

Page 316: ...TOFLIGHT TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 22 00 00 GENERAL 2F3 A 8 82 22 10 00 NON PIPER A F C S EQUIPMENT CONTACTS 2F3 A 8 8 Piper A F C S Equipment D...

Page 317: ...anufacturers to obtain service direction parts support and service literature Bendix Avionics Division 2100 N W 62nd Street Fort Lauderdale Fla 33310 305 776 4100 TWX 5109559884 Collins General Aviati...

Page 318: ...CHAPTER COMMUNICATIONS 2F4...

Page 319: ...00 GENERAL 2F6 23 20 00 DATA TRANSMISSION AND AUTOMATIC CALLING 2F6 23 21 00 Emergency Locator Transmitter 2F6 23 21 01 Description 2F6 23 21 02 Battery Removal and Installation 2F6 23 21 03 Descript...

Page 320: ...ELT from its mounting bracket by releasing the latch on the strap and sliding the ELT off the bracket 5 Extend the portable antenna See Figure 23 1 6 Unscrew the four screws that hold the control hea...

Page 321: ...should be no longer than three audio sweeps 2 If the antenna is removed a dummy load should be substituted during the test 3 Test should be conducted only within the time period made up of the first...

Page 322: ...on WARNING Whenever the unit is checked by moving the transmitter ON ARM OFF switchfrom theARM to theON position it must then be moved to the OFF position if there is one before reverting to the ARM p...

Page 323: ...PSOUT ON OF CHANNEL AND DOWN VIEW PIN PULL TAB STOP VIEW TO EXTEND TO FULL LENGTH C Figure 23 1 Portable Folding Antenna Narco CONTACT PORTABLE ANTENNA BLADE SEPARATOR PORTABLE NOT ANTENNA MAKING CONT...

Page 324: ...CHAPTER ELECTRICAL POWER 2F10...

Page 325: ...32 00 Overhaul 2F22 24 32 01 Lear Siegler 2F22 24 32 02 Disassembly 2F22 24 32 03 Cleaning 2F23 24 32 04 Removing Carbon Dust from Auxilec 8013C Starter Generator 2F24 A 3 84 24 32 05 Inspection 2G2 2...

Page 326: ...ture Sensor 2H2 24 40 00 EXTERNAL POWER 2H3 24 41 00 Emergency Starting through External Power Receptacle 2H3 IR 3 84 24 50 00 ELECTRICAL LOAD DISTRIBUTION 2H4 24 51 00 Overload Sensor 2H4 24 51 01 De...

Page 327: ...the aircraft The five basic electrical systembuses are also connected to the tie bus The mode of operation of the DC Starter Generator isselected by utiliing the Left and or Right Starter Generator s...

Page 328: ...rcuited or open Replace the stator and stator windings housing assembly Improperly seated Check brush seats and brushes increase brush run in time Eccentric commutator Refinish commutator Excessive sp...

Page 329: ...lace brush holder assemblies Noisy operation Rough bearings Replace bearings Scored or worn drive Replace drive shaft splines Armature rubbing in stator Repair or replace defective parts Fan blades be...

Page 330: ...r accumulation in generator air inlet ducting Wrong load applied during Check testing procedure testing and correct condition Starter generator fails Short circuited or open Replace stator and hous st...

Page 331: ...D cont Intermittent oper Short circuited coil Replace coil Clean and ation Loose electrical con tighten electrical con nection nections Plunger binding See remedy pertaining to Plunger binding under D...

Page 332: ...cks valve in the air inlet duct which regulates direct airflow and a four bladed fan which is part of the unit Cooling is obtained by routing the outside ram air through the air inlet duct which is th...

Page 333: ...27 SCREW 48 STATOR 9 SCREW 28 BEARING 49 INSTRUCTION 10 FAN 29 SCREW DECAL 11 LOCKNUT 30 BRUSH HOLDER 50 IDENTIFICATION 12 DRIVE SHAFT 31 NUT PLATE 13 PLATE DAMPENER 32 WASHER 51 SCREW 13A HUB DAMPEN...

Page 334: ...26 DISK DAMPER 42 KEY 1 SCREW 2 BRUSH BAND 18 DISK DAMPER 3 NUT 19 BALL BEARING FLANGE 45 MOUNTING CLAMPSHER 4 FLAT WASHER 0 START GENERATOR KEY 36 SECTURE 5 NUT 21 SCREW 37 CLAMP 6 FLATWASHER 22 CLA...

Page 335: ...the airplane 9 Connect electrical lead previously removed to C terminal stud on Starter Generator ADJUSTMENTS The only adjustment necessary to maintain the generator system is the adjustment of the v...

Page 336: ...nation C C 1 Self cooled 2 Blast cooled OVERHAUL When repairing the unit complete disassembly may not be required In some cases it will only be necessary to perform those operations which are required...

Page 337: ...armature shaft Remove the bearing from armature by using a suitable bearing puller then remove the disc baffle from the armature 9 Remove the screws securing the bearing retainer and remove bearing r...

Page 338: ...nozzle of the tool between the radial leads connecting the bars of the commutator to the conductors up to the black band on the tool nozzle as shown in Figure 24 2a B When the tool has been inserted...

Page 339: ...TRAP 4 BEARING 5 COMMUTATOR BEARING HOUSING 6 ARMATURE 7 DRIVE SHAFT 8 STATORAND HOUSING ASSY Figure 24 2a Position of Auxilec Tool for Blowing out Carbon Dust from Auxilec 8013C Starter Generator THI...

Page 340: ...n 0 830 inch Replace if beyond repair Drive Shaft 12 Magnaflux inspect per MIL 1 6868 for cracks Visually inspect for broken or damaged splines and spline wear To measure spline wear on the large spli...

Page 341: ...s accurately set up and adjusted Remove only enough material to clean and true up the commutator surface Replace the armature if it has to be turned to less than a diameter of 2 055 inches Hold commut...

Page 342: ...emaining brush holders 6 When replacing brushes no brush run in is required 7 A unit with reversed polarity in the output voltage may be corrected by flashing the field as in the procedure below CAUTI...

Page 343: ...washers lock washers and screws Make certain end bell is fully seated on bearing NOTE Items 16 and 17 of Figure 24 1 not used on quick disconnect model 20348 006 7 Install dampener back plate on arma...

Page 344: ...5 Special Purpose Equipment 5 Remove damper disk using the extractor P N A 1003 fitted with end piece P N 4B09378 and pull disk out Refer to Chapter 95 Special Purpose Equipment 6 To remove the fan un...

Page 345: ...A Clean the windings with a brush in a container of Aliphatic Naphtha Grade F NOTE Particular attention should be given to the winding base B Blow dry the washed windings with a jet of dry compressed...

Page 346: ...cks and loose or damaged terminals B Check for shorts between terminals C Replace if defective REASSEMBLY Refer to Figure 24 2 1 To reassemble the stator carefully release the stator connections then...

Page 347: ...18 Fold washer lugs over screws in order to safety them 19 To install the fan fit the key P N E3392 through machine nose section inarmature splines to keep it from rotating Refer to Chapter 95 Specia...

Page 348: ...crews to 0 150 m daN 13 inch pounds 28 Install drive shaft fitted with damper disk into stator flange mounting side then engage its splines on those of the armature NOTE Damper disk must be mating on...

Page 349: ...disk then tighten nut to obtain the dimension C as shown in Figure 24 6 NOTE When tightening nut ascertain that thefibrous damper disk remains inside the damper disk recess 36 Ascertain that damper di...

Page 350: ...ch pounds 40 Lockwire screws 34 two by two and brush band screw with 0 6 mm diameter annealed stainless steel Refer to Figure 24 2 NOTE The electrical connections torque valuesfor terminals A and D ar...

Page 351: ...ith key P N E3392 in a counterclockwise direction seen from driving side Refer to Chapter 95 Special Purpose Equipment NOTE Turnthe rotor regularly and evenly until brush contact surface is 100 Check...

Page 352: ...in the circumference direction and 100 minimum in the axial direction If not pursue the brush running in operation until these values are reached M Disconnect the instrument N Blow carbon dust out of...

Page 353: ...re is grounded and must be replaced C To test the stator assembly use the same circuit as before and touch one lead to the frame and the other to terminal A If lamp lights stator is grounded and must...

Page 354: ...ame and the other to the leads removed from terminal block The leads from the terminal block must beremoved from studs due to the embedded capacitors connected to ground The unit shall not be shorted...

Page 355: ...eed to step 6 6 Reset right main bus circuit breaker open in step 5 7 Avionics bus should be dead no electrical power if the avionics bus is powered the bus feed diode from the right side right main i...

Page 356: ...mponents reverse of removal instructions CLEANING BATTERY 1 Remove all accumulated contamination from the battery exterior with a stiff bristle brush Don use a metal brush or abrasive materials 2 Wipe...

Page 357: ...drying apply a high quality aircraft wax to the entire area CLEANING AND RECHARGING ACID RECOVERY JAR 1 Unscrew the bottom and separate from the top of the jar 2 Remove jar pad and empty contents int...

Page 358: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL Figure 24 10a Lead Acid Battery Installation 24 33 06 Page 24 32 2G20 Revised March 5 1984...

Page 359: ...ity electrolyte Repeat this step if after one hour of charging thespecific gravity isstill too low DO NOT ADJUST A CELL THAT DOES NOT GAS To adjust high specific gravity charge the battery see Chargin...

Page 360: ...BATTERY DISCHARGE The capacity of a storage battery is measured in units of ampere hours which is the product of the electrical current in amperes multiplied by the time in hours Although current may...

Page 361: ...urs is the rate of discharge to 1 75 volts per cell EMERGENCY CAPACITY AMP The amperes shown is the rate of discharge for 25 minutes to a cut off voltage of 1 75 volts per cell COLD TEMP CRANKING The...

Page 362: ...follows Saft America Inc Operating and Maintenance Manual P N DC 3 01 78 3176 5 latest revision and Marathon Battery Marathon battery instruction manual P N BA 89 Refer to front of this maintanenance...

Page 363: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL SAFT THERMOSTAT B169 FUSEHOLDER I li1 i 1 MARATHON Figure 24 11 Cell Layout Nickel Cadmium Battery 24 33 10 Page 24 37 2H1 Revised March 5 1984 2H1...

Page 364: ...the inline connector 4 Put electrical connectoron battery with the symbols ontheconnector on top and the symbols on the connector on the bottom Secure by tightening knob on connector 5 Secure knob by...

Page 365: ...actor will auto matically energize immediately applying power to all aircraft busses 2 Turn OFF battery master switch 3 Turn OFF all electrical loads as in a normal start 4 Connect a A P U unit to the...

Page 366: ...tem the overload sensor through a slaved mechanical switch would open the generator field control circuit breaker There is one overload sensor for each starter generator REMOVAL OF OVERLOAD SENSOR The...

Page 367: ...OL PANEL ELECTRO DELTA NOTE It is necessary to fabricate test equipment per the following schematic provided by Electro Delta Inc Figure 24 12 1 A digital voltmeter and regulated D C power supply are...

Page 368: ...d verify both L C and FIELD lights extinguish and release 0 voltage test switch 10 Repeat steps 7 and 8 11 Depress REMOTE TRIP switch SW 2 and again verify both L C and FIELD lights extinguish 12 Repe...

Page 369: ...STIVE TYPE ELEMENT INT 2 26 9 INTAKE 2 30 RESISTIVE TYPE ELEMENT INT 21 2 INTAKE 3 30 RESISTIVE TYPE ELEMENT INT 19 9 RIGHT LIP DEICE INTAKE I 30 RESISTIVE TYPE ELEMENT INT 2 269 INTAKE 2 30 RESISTIVE...

Page 370: ...TO IGNITION RELAY INT 5 LEFT IGNITION SOLID STATE INT RIGHT IGNITION 5 SOLID STATE INT 350 LEFT FLEL PRESSURE 3 INDICATOR TRANSDUCER CONT RIGHT FL EL PRESSLRE INDICATOR TRANSDUCER CONT 40 LEFT FLEL FL...

Page 371: ...LENOID L L SOLENOID GEAR DOWN INT 50 LOCK SOLENOID FLIGHT INT 1 10 RELAY GROUND ONLY INT 20 LAMP IN TRANSIT INT 04 PROP SYNC SOLID STATE CONT LEFT H T G BETA 5 LOCK PITCH SOLENOID CONT H T G SOLENOID...

Page 372: ...COLLISION STROBES AND PWR SUPPLY CONT STROBES LEFT ANTI COLLISION STROBES AND PWR SUPPLY CONT STROBES RIGHT LANDING LIGHT 10 LAMP INT 2 SOLENOID INT POSITION LIGHTS 75 LEFT LAMP CONT RIGHT LAMP CONT T...

Page 373: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2H11...

Page 374: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2H12...

Page 375: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2H13...

Page 376: ...CHAPTER EQUIPMENT FURNISHINGS 2H14...

Page 377: ...H 16 25 21 01 Removal 2H 16 25 21 02 Installation 2H 16 25 22 00 Passenger Seats 2H 16 25 22 01 Remoal 2H 16 25 22 02 Installation 2H 16 25 23 00 Shoulder Harness Inertial Reel Adjustment 2H18 25 50 0...

Page 378: ...tracks and slide the curtains off the curtain tracks 2 The forward and aft divider curtain tracks can be removed by releasing the remaining three and five attachment screws respectively INSTALLATION 1...

Page 379: ...MANUAL 3202 THIRD AND FOURTHPASSENGER SEATS FORWARDFACING 6 FIFTHTHRUNINTH PASSENGER SEATS FORWARDFACING 7 TENTHAND ELEVENTH PASSENGERSEATS FORWARD FACING Figure 25 1 Interior Arrangement 25 22 02 Pag...

Page 380: ...selage structure A cargo net and tie down straps anchored to the barriers and tie down rings positioned on the seat tracks facilitate securing cargo of various bulks for appropriate weight distributio...

Page 381: ...0 C 200 400 D 200 1800 2000 E 200 900 TOTAL F 100 440 G 30 150 EACH MAXIMUM TIEDOWN CAPACITY PER FOOT OF TRACK 200 LBS PER TRACK 900 LBS PER TIEDOWN RING 200 LBS CARGO MUST BE LOADED WITHINTHE WEIGHT...

Page 382: ...E TIE DOWN RING 6 CARGO STRAP 7 CARGO STRAP TIE DOWN RING 8 CARGO STRAP ATTACHMENTRING 9 CARGO BARRIERPIN 10 CARGO BARRIERTRIM COVER 11 CARGO BARRIERATTACHMENT FITTING 12 ROLL PIN 13 CARGO EQUIPMENT S...

Page 383: ...o Chapter 33 Lights for information on the cargo pod lighting REMOVAL OF CARGO POD I Place suitable supports beneath the cargo pod to prevent it from dropping while the attachment screws are being rem...

Page 384: ...CHAPTER FIRE PROTECTION 2H22...

Page 385: ...ISHING 211 26 20 01 General 211 26 20 02 Description and Operation 211 26 21 00 Testing Extinguishing System 211 26 22 00 Fire Extinguisher Bottle 213 26 22 01 Removal of Fire Extinguisher Bottle 213...

Page 386: ...e seal inthe hot section and one is located at the bottom of the rear fire seal in the accessory section The thermal units actuate at a temperature of 450 F Whenever the contacts in any one of the the...

Page 387: ...he cockpit is actuated the firing squib in the discharge valve is detonated which in turn punctures the seal in the discharge valve allowing the release of the extinguishing agent through the pipes Th...

Page 388: ...9 Repeat Steps 1 through 9 for opposite engine 10 A pressure check of the fire extinguisher containers should be made periodically to determine that the pressure is between the minimum and maximum li...

Page 389: ...with care to avoid damaging the seal Do not bring any electricalcurrent in contact with the terminals on the squib assembly of a loaded unit or accidental detonation could result 4 Disconnect the dis...

Page 390: ...the fire seal fitting 5 Ascertain the placement of the discharge nozzles per the dimension shown in Figure 26 3 It is important that the nozzles be positioned as shown to obtain proper dispersal of th...

Page 391: ...ection tag is present and has been updated B Check that the locking ring is firmly in place and has not been tampered with C Check for cleanliness dents scratches damage and corrosion Iffound take ext...

Page 392: ...CHAPTER FLIGHT CONTROLS 216...

Page 393: ...Aileron Controls 2J13 27 14 00 Aileron Trim Control Pedestal 2J 14 27 14 01 Removal of Aileron Trim Control Pedestal 2J 14 27 14 02 Wrapping Control Pedestal Aileron Trim Drum 2J15 A 3 84 27 14 03 Ins...

Page 394: ...2 01 Removal of Elevator Bellcrank 2K10 27 32 02 Installation of Elevator Bellcrank 2K13 27 33 00 Rigging and Adjustment of Elevator Controls 2K13 R 3 84 27 34 00 Elevator Trim Control Pedestal 2K 14...

Page 395: ...ps 2L6 27 55 00 Flap Position Sender 2L10 27 55 01 Removal of Flap Position Sender 2L10 27 55 02 Installation of Flap Position Sender 2L10 27 55 03 Rigging and Adjustment of Flap Position Sender 2LI I...

Page 396: ...icular control surface As the trim control wheels are rotated they in turn rotate the mating drums at the control surfaces to actuate the particular trim tab A sender unit is installed at each trim ta...

Page 397: ...e tension too high Adjust cable tension Control column hori Adjust chain tension zontal chain improperly adjusted Pulleys binding or Replace binding pulleys rubbing and or provide clearance between pu...

Page 398: ...l control wheel and control control cables travel cables AILERON TRIM CONTROL SYSTEM Lost motion between trim Cable tension too low Adjust cable tension control wheel and trim tab Cables not in place...

Page 399: ...ONTROL SYSTEM Lost motion between Cable tension too low Adjust cable tension control wheel and ele vator Linkage loose or worn Check linkage and tighten or replace Broken pulley Replace pulley Cables...

Page 400: ...l Elevator cables incor Rig cables cannot be obtained by rectly rigged adjusting elevator arm stops ELEVATOR TRIM CONTROL SYSTEM Lost motion between trim Cable tension too low Adjust cables control wh...

Page 401: ...m indicator unit not Adjust unit dicate correct trim posi adjusted properly tion RUDDER CONTROL SYSTEM Lost motion between Cable tension too low Adjust cable tension rudder pedals and rudder Linkage l...

Page 402: ...ellcrank stop Rig rudder bellcrank stop incorrectly adjusted Nose wheel contacts stops Rig wheel contacts stops before rudder RUDDER TRIM CONTROL SYSTEM Lost motion between trim Cable tension too low...

Page 403: ...ped rigging Trim indicator fails to in Trim indicator unit not Adjust indicator unit dicate correct trim adjusted properly position FLAP CONTROL SYSTEM Flaps fail to extend or re Battery switch off Tu...

Page 404: ...solate cause and repair Flaps fail to retract Up limit switch incor Adjust flap completely rectly adjusted Flaps do not extend Down limit switch in Adjust limit switch completely correctly adjusted Fl...

Page 405: ...ing Check and repair wiring Battery switch off Turn switch on Circuit breaker open Reset circuit breaker Sender unit ground open Check ground connection Annunciator light ON Amplifier component Replac...

Page 406: ...e and service actuator Motor bearing failure Repair motor Motor short circuit Repair motor System shutdown Improper system hookup Perform rigging electrical tests Malfunctioning amplifier Replace ampl...

Page 407: ...nection failure Replace shaft or con nection Outboard flexshaft and Replace the required item or coupling failure Frozen screwjack Worm bearing failure Remove and service actuator compression bearing...

Page 408: ...vice the control box No flap movement Flap control box Service the control box Lever shaft failure Locking pin failure Gearing failure Flexshaft or coupling Replace worn part failure Open circuit Chec...

Page 409: ...Replace amplifier flaps operate Annunciator light on Flap motor circuit breaker Reset circuit breaker with flaps inoperative pulled or tripped Flaps asymmetric Check and rerig flaps Potentiometer fail...

Page 410: ...efer to Chart 2702 NOTE Whenevertheelevatorcontrolsystem is serviced africtioncheckof thesystem must be accomplished in accordancewith instructions given in Elevator Control System Friction Measuremen...

Page 411: ...DAMAGE HERE WRONG DAMAGE HERE IMPROPER TOOL RESULTING IN LOCKED BALL A SPECIAL WRENCH MAY BE REQUIRED WITH A LONG THROAT ONLY CORRECT METHOD Figure 27 1 Correct Method of Installing Rod End Bearings...

Page 412: ...ller fitting D Cut the wire that safeties the cap bolts that secure the collar to the roller fitting Remove the bearing housing from the fitting E Disassemble the rollers from the fitting Note the num...

Page 413: ...anel INSTALLATION OF CONTROL COLUMN Refer to Figure 27 3 1 Installation of the control column torque assembly may be accomplished by the following procedure A Position but do not attach control arms o...

Page 414: ...E TORQUE 44 CONTROLTUBE LEFT 74 BOLTASSY 15 BEARING BLOCK 45 SCREW ADJUSTMENT 75 HOUSING SPROCKET 16 ARM CONTROL R I 46 BLOCK 76 BUSHING 17 BOLTASSY AND ROLL PIN 47 HOUSING GUIDE ASSY 77 NUT KAYNAR 18...

Page 415: ...T 1040 MAINTENANCE MANUAL 174 171 31 21 5 24 22 60 61 23 25 24 13 62 24 68 70 69 68 70 SKETCH A SKETCH B SKETCH C SKETCH D Figure 27 3 Control Column Installation cont 27 03 02 Page 27 21 Revised Mar...

Page 416: ...ers c Install the bearing housing with bearings on the roller housing Install collar and cap bolts Rotate the collar tight against the bearing housing tighten cap bolts and safety D Ascertain that the...

Page 417: ...and rotate the tube 180 Reinstall bolts torque and safety 7 Adjust the control wheel tube slides at the instrument panel by tightening the adjustment screw to remove any play in the tube without rest...

Page 418: ...ckle separating the ends at the forward end of the aileron bellcrank C Remove the cable guard pins at wing station 29 00 and 150 00and within the fuselage at station 164 50 and 168 50 Remove the fairl...

Page 419: ...forward control cable turnbuckle within the fuselage at station 100 00 D If balance cable is installed install the cable guard pins at wing stations 29 00 and 150 00 and fuselage stations 164 50 and 1...

Page 420: ...LE 16 TURNBUCKLES 19 NUT JAM 11 TRIM CABLE 1 NUT JAM 13 TRIM SCREW ASSY 41 BOLT ASSEMBLY 4 BRACKET 14 PULLEY 43 BRACKET 15 CABLE CONTROL R 36 CABLE 16 CABLE BALANCE R 31 CONNECTOR 41 NUT JAM 56 BOLTSA...

Page 421: ...NANCE MANUAL SKETCH B FUSELAGE STATION 274 00 SKETCH C WING STSTION 147 50 SKETCH D FUSELAGE STSTION 125 21 S KETC H Figure 27 7 Aileron and Aileron Trim Controls cont 27 11 02 Page 27 27 2J11 Interim...

Page 422: ...assembly 2 Relieve cable tension from the control system by rotating one of the turnbuckles attached to the bellcrank 3 Disconnect the turnbuckle ends from the forward and aft ends of the bellcrank 4...

Page 423: ...tool between the bellcrank mounting brackets and over the end of the bolt from which the nut was removed It may be necessary to loosen one of the primary control cables or the balance cable D Positio...

Page 424: ...aileron and establish neutral or zero on the protractor Remove the tools holding the aileron bellcranks in neutral replace nuts and safety Adjust the bellcrank stop bolts to the specific aileron trav...

Page 425: ...later installing and wrapping the cable on the drum 2 With the drum housing bracket firmly held remove one of the cable guard bolts from the housing bracket 3 Remove the drum shaft from the trim screw...

Page 426: ...aileron cable tension per Figure 27 11 and check rigging and adjustment 8 If the trim cables from the screw assembly within the wing are installed connect the cable ends at the turnbuckles at wing sta...

Page 427: ...IM CONTROL 2 RUDDER TRIM CONTROL 4 ELEVATOR TRIM SCREW 14 GEAR BOX 3 TRIM POSITION INDICATOR 9 PIN AND COTTER PIN 4 AILERON TRIM CONTROL 10 SLEEVE 5 RUDDER TRIM SCREW 11 BUSHING AND PLATE 6 AILERON TR...

Page 428: ...RPLANESWITHOUT AUTOPILOT BRIDLECABLESATTACHED REFERTO 20 1 APPROPRIATE AUTOPILOT SERVICE Cord Line Level Neutral Poition MANUAL FOR PROPER CABLE TEN SIONS WHEN ATTACHING BRIDLE CABLES Figure 27 11 Ail...

Page 429: ...ps on the trim screw and the cables blocked to prevent them from unwrapping 2 Position the screw assembly in the wing install the attachment cap bolts and torque 3 Draw the cables through the wing and...

Page 430: ...le slot in the trim drum Insure that the center of the cable is in line with the center of the cable slot Install the cable lockpin C Hold the drum with its base down Wrap the cable that leads from th...

Page 431: ...check the minimum number of cable wraps left on the drum Minimum allowable is one and one quarter turns 6 Check rigging and adjustment of trim indicator RUDDER AND TAB The rudder and tab system consis...

Page 432: ...CH D 10 TURNBUCKLE INTERCONNECTING 35 BOLTASSEMBLY 11 SPRING SLACK TAKE UP 36 RUDDER TUBE 12 SPRING SLACK CONTROL 37 BOLT ASSEMBLY 13 BALL CLAMP 38 BOLT ASSEMBLY 14 SPRING TENSION 39 CABLE END 15 PULL...

Page 433: ...T 1040 MAINTENANCE MANUAL 3153C C423 SKETCH C SKETCH D SKETCH Figure27 13 Rudder and udder Trim Controls cont SKETCH G Figure 27 13 Rudder and Rudder Trim Controls cont 27 21 01 Page 27 39 Issued Marc...

Page 434: ...of the turnbuckles at fuselage station 100 00 4 Mark one end of the rudder sector and cable end to facilitate installation and disconnect the cables from the rudder sector ends 5 Unbolt the rudder sec...

Page 435: ...move the left pilot s seat and the floor panel to the left of the control pedestal 2 Relieve the tension from the rudder control cables by loosening one of the cable turnbuckles 3 Disconnect the rudde...

Page 436: ...s of 012 02 P N 81102 35 018 02 P N 81102 36 and 032 P N 81102 37 5 Lubricate and slide the torque tube through side of the fuselage and right bearing far enough to slide the right retainer collar on...

Page 437: ...RQUETUBE 21 BEARINGBLOCK CHANNEL 7 BOLT 22 MOUNTING BRACKET 35 TORQUETUBE GUARD 8 ROLL PIN BOLT 23 PLATE 36 MACHINE SCREWS 9 CABLE END 24 ROD AND NUTS 10 BOLT 25 CONTROLCABLE 37 SCREWS NUTS AND 11 BOL...

Page 438: ...e elevator torque tube and slide it to the left until the centerline on thejig plate aligns with the centerline of the airplane D Set a bubble protractor to 29 28 and position it on the centerline of...

Page 439: ...m the control pedestal WRAPPING RUDDER TRIM DRUM CONTROL PEDESTAL 1 Mark the end of thedrum toward the base of the housing bracketfora reference when later installing and wrapping the cable on the dru...

Page 440: ...ly on its mounting bracket Install attachments bolts and secure 3 Draw the cables from the pedestal through the fuselage to the aft section of the fuselage 4 If the trim cables from the rudder are ins...

Page 441: ...locked to prevent them from unwrapping 2 Position the screw assembly in the vertical fin install the attachment bolts and secure 3 Draw the cables through the fin into fuselage and connect them at the...

Page 442: ...rum There should be a 20 16 inch difference in the length of the unwrapped cable as it comes out of the trim drum The shorter end of the cable should be that end which comes out of the lower end of th...

Page 443: ...system consists of control column pulleys springs bellcrank control rod elevator torque tube assembly and interconnecting cables This section contains information for the maintenance repair rigging a...

Page 444: ...of the control sector C If aft control cables are installed connect the cables at station 110 50 D Install cable guard pins at forward pulley cluster 2 The control cables that route aft beginning at...

Page 445: ...38 ROD END 9 RUB BLOCK 24 BOLT PIVOT 39 ROD CABLE GUARD 10 CONTROLCABLE 25 PULLEY 40 CENTERCABLE 11 CONTROLCABLE 26 ROD END 41 TURNBUCKLE 12 TURNBUCKLE 27 BOLT ASSEMBLY 42 SPRING 13 TRIM CABLE 28 JAM...

Page 446: ...TIONS ENDNO 2 VIEW A A END NO 1 3219 NOTE THERE MUST BE TWO SAFETY END NO 1 CLIPS NAS651 16S PIPER PART NO 454 867 INSTALLED PER EACH STA TURNBUCKLE 362 00 RIGHT HAND 1 31 TURNBUCKLE ENDNO 2 12 19 TO...

Page 447: ...ith trailing edge of the elevator This tool may be fabricated from dimensions given in Chapter 95 3 With the elevator in neutral position check or adjust the elevator bellcrank for neutral The bell cr...

Page 448: ...els tail cone and seats ELEVATOR TRIM CONTROL PEDESTAL The elevator trim system consists of an elevator trim wheel and trim screw mounted in the control pedestal pulleys and trim screw connecting rods...

Page 449: ...ables at the trim screw assembly within the control pedestal and the aft cables at bulkhead 317 75 to prevent the cables from unwrapping from their drums by one of the methods shown in Figure 27 6 If...

Page 450: ...tor trim cable on the forward trim drum located beneath the control pedestal A Locate the center of the cable B Insert the cable into the cable slot in the trim drum Insure that the center of the cabl...

Page 451: ...ileron control knob and secure knob with roll pin 10 Install access plates panels and seats ELEVATOR TRIM ELEVATOR REMOVAL OF ELEVATOR TRIM ELEVATOR Refer to Figure 27 18 1 Remove the access plates lo...

Page 452: ...s between the lower surface of the plate and the boss on the bracket Insure there is 07 inch between the upper surface of the retainer and the lower surface of the bushing Refer to Figure 27 21b CHART...

Page 453: ...NUMBER END NUMBER 2 END NUM 2 1 BUSHING 2 HOUSING BRACKET 3 RETAINER END 1 AFTERWRAPPING END 2 AFTERWRAPPING D152 END 2 WRAP DIRECTION END 2 BEFOREWRAPPING 12 TURNS END 1 WRAP DIRECTION END 1 BEFOREW...

Page 454: ...ND ADJUSTMENT OF ELEVATOR TRIM 1 To adjust the elevator trim the following steps should be accomplished during installation or as an adjustment check A Remove the access panels on the left and right s...

Page 455: ...gures 27 23 and 27 24 LH 2091 Thewingflapcontrol systemprovidescontinuouscontrol and monitoringof flappositionand condition over its full range In addition to the limiting of both up and down overtrav...

Page 456: ...LY 12 WIRE SAFETY MS20995C32 13 MOUNTING BRACKET MOTOR 14 ROD LINKAGE 19 SWITCH DOWN LIMIT 24 ADJUSTMENT BOLT UP LIMIT 15 BUSHING AND SCREW ASSY 20 SHAFT SENDER 26 ADJUSTMENT BOLT DOWN LI 16 FLAP HORN...

Page 457: ...MAINTENANCE MANUAL FAULT LIGHT LEFT FLEXIBLE SHAFT UP LIMIT SWITCH LEFT TRANSMISSION DOWN LIMIT SWITCH RHEOSTAT LINKAGE LEFT CONTROL RHEOSTAT Figure 27 24 Flap System Diagram 27 50 01 Page 27 63 Revi...

Page 458: ...n forward side of the fuselage bulkhead at station 174 00 2 Disconnect the electrical leads from the motor 3 Cut the safety wire and disconnect the flexible drive shaft ends from the motor 4 Remove th...

Page 459: ...HEX HEAD 5 END BELL ASSY FRONT 6 BRUSHASSY 7 SPRING BRUSH INSULATOR ASSY 15 10 STUD CONTACT 11 NUT HEX EARLYMOTORS 12 WASHER LOCK 13 SHOULDERWASHER 14 ENDBELL 15 BEARING BALL 16 WASHER SPRING 17 ARMAT...

Page 460: ...tepped around commutator B Insulation resistance between commutator and shaft should be 10megohm minimum at 85v ASSEMBLY OF FLAP ACTUATOR MOTOR Refer to Figure 27 25 1 Assemble shoulder washers contac...

Page 461: ...ACTUATOR SHAFT Refer to Figure 27 23 REMOVAL OF FLEXIBLE ACTUATOR SHAFT Refer to Figure 27 23 1 Remove the center floor panel located in the main cabin area 2 Remove the right and or left row of seat...

Page 462: ...nd adjustments per instructions given in this section 5 Install the access plates panels clamps grommets and seats FLAP TRANSMISSION REMOVAL OF FLAP TRANSMISSION Refer to Figure 27 23 1 Lower the flap...

Page 463: ...irection Do not force the pliers 5 Place a six inch ruler along the skin surface as shown in ViewB and measure the overall distance the pliers move 6 Should this dimension exceed 30 of an inch replace...

Page 464: ...tion VCR Voltage difference between VC VR at flap up position VRL Voltage difference between RL RR RT2 Amplifier Trimmer Adjustment Left RT3 Amplifier Trimmer Adjustment Right The Control rheostat ope...

Page 465: ...manually moving the flap adjust the UP limit actuating bolt so that the switch is actuated with 03 inch maximum gap between the rollers and the end of the flap track slots See Figure 27 27 Sketch B N...

Page 466: ...X XX X XX T The values at the DOWN position have already been established for VC VLand VR in Step O preceding At this time enter the readings for VC VL and VR at the UP position The work sheet might...

Page 467: ...ER AIRCRAFT T 1040 MAINTENANCE MANUAL A404 ACTUATOR ARM ROD LINKAGE SKETCH A 03 UP LIMIT FLAP TRACK DOWN LIMIT SKETCH B Figure 27 27 Flap Rigging Adjustments 27 54 00 Page 27 73 2L9 Revised March 5 19...

Page 468: ...r stroke and position indication place the positive probe of the digital voltmeter in RR at the amplifier and the negative lead in RL Select the flaps full DOWN and monitor the voltage throughout the...

Page 469: ...when the flaps are lowered to 15 1 lift flap trailing edge to obtain angle measurement 5 Install the access plates FLAP CONTROL BOX REMOVAL OF FLAP CONTROL BOX 1 Remove the knob from the control box...

Page 470: ...the u or down relay and run the motor II Check the 27 5 volt power at the drive motors whileanother person is energizing relays K1and K2 If 27 5 volts is not present at the drive motor the contacts o...

Page 471: ...INTENANCE MANUAL AIRCRAFT ELECTRICALSYSTEM MOTOR CB 27 5V _______________1 _____ 9 ______A_ __Rll 12K I 430 K 3 __43_0 Figure 27 28 Amplifier Electrical Schematic Calco P N 8482 27 58 00 Page 27 77 2I...

Page 472: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL UPRELAY...

Page 473: ...ted to the channel above the access panel at station 64 5 This time delay unit assures a horn sound when the lift detector switch closes and for four seconds after the detector switches opens A heated...

Page 474: ...o late move the switch up If the stall warning comes on too early move the switch down Retighten the screws after making any adjustments CA UTION Never try to adjust the switch by bending the vane The...

Page 475: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL GRIDS 2L17 THRU 2L24 INTENTIONALLY LEFT BLANK 2L17...

Page 476: ...MAINTENANCE MANUAL MAINTENANCE MANUAL CARD 3 OF 5 PA 31T3 T1040 PIPER AIRCRAFT CORPORATION PART NUMBER 761 765 3A1...

Page 477: ...en down into Sub System Sections These sections are identified by the second element of the standardized numbering system The number 40 of the basic number series 32 40 00 is for the Wheels and Brakes...

Page 478: ...te list of Charts is for all fiche in this set following list of Illustrations 4 A complete list of paragraph titles and appropriate Grid location numbers is given at the beginning of each Chapter rel...

Page 479: ...6 3 IR900313 March 13 1990 2 IR941012 October 12 1994 1 and 3 INTERIM REVISION Revisions appear in Chapter 5 of card 1 and Chapter 30 or card 3 Please dispose of your current cards 1 and 3 and replace...

Page 480: ...P N DC 3176 5A Marathon Nickel Cadmium Battery instruction Manual P N BA 89 DE ICE SYSTEM PROPELLERS B F Goodrich Electrothermal Propeller Deice Maintenance Manual P N 68 04 712 Latest Revision B F G...

Page 481: ...Manual All Models P N 23700 Lear Siegler Inc Overhaul Manual Series 23048 P N 23202 PIPER PUBLICATIONS PARTS CATALOG 761 761 Piper Aircraft Corporation 820 E Bald Eagle Street Lock Haven Pennsylvania...

Page 482: ...0497 Air Conditioning System Electronic TIF Instruments Leak Detector 3661 N W 74th Street Miami Florida 33147 305 696 7100 Autopilot Avionics Edo Corporation Avionics Division P O Box 610 Municipal...

Page 483: ...102 Bethesda Maryland 20034 301 229 5000 Electrical Relays Leach Corporation 5915 Avalon Boulevard Los Angeles California 90003 213 232 8221 Emergency Locator Transmitter Narco Avionics Inc 270 Comme...

Page 484: ...sion 1214Exposition Boulevard Los Angeles California 90064 213 774 3230 Instruments Aerosonic Corporation 1212 N Hercules Avenue Clearwater Florida 33515 813 461 3000 Landing Gear Hydraulic Actuators...

Page 485: ...Company Drake and Lemay Roads Fort Collins Colorado 80521 303 482 5811 Starter Generator Auxilec Incorporated One Willow Park Center Farmingdale New York 11735 516 694 1441 Lear Siegler Incorporated...

Page 486: ...1F1 10 PARKING AND MOORING 1F5 11 REQUIRED PLACARDS 1F8 12 SERVICING 1F13 20 STANDARD PRACTICES AIRFRAME 1G21 21 ENVIRONMENTAL SYSTEM 2B1 22 AUTOFLIGHT 2F1 23 COMMUNICATIONS 2F4 24 ELECTRICAL POWER 2...

Page 487: ...53 FUSELAGE 4G 16 55 STABILIZERS 4G19 56 WINDOWS 4H 15 57 WINGS 411 61 PROPELLER 4117 70 STANDARD PRACTICES ENGINES 4K5 71 POWER PLANT 4K8 72 ENGINE TURBO PROP 4L 1 73 ENGINE FUEL SYSTEM 4L4 74 IGNITI...

Page 488: ...er Doors 1G11 12 9 Lubrication Chart Cabin Door Baggage Door Seats 1G12 12 10 Lubrication Chart Air Conditioner Quill Shaft 1G12 20 1 Torque Wrench Extension 1H1 20 2 Correct Method of Installing Rod...

Page 489: ...34 Installing Pulley and Drive Plate Bearing 2E8 21 35 Installing Pulley and Drive Plate 2E8 21 36 Removing Coil Housing Retaining Ring 2E9 21 36a Positioning Sankyo Compressor Internal Parts 2E11 21...

Page 490: ...ation of Aileron Rigging Tool 2J13 27 9a Wrapping Control Pedestal AileronTrim Drum 2J16 27 10 Trim Controls Installation 2J17 27 11 Aileron Control Travels and Cable Tension 2J18 27 12 Safety Wiring...

Page 491: ...mp 3C 10 28 15 Test Equipment Hookup 3C15 28 16 Alternate Indicator Bench Test Hookup 3C18 28 17 Fuel Gauge Adjustment 3C19 29 1 Schematic Diagram Hydraulic System 3D20 29 2 Schematic of Power Pack El...

Page 492: ...of Dial Indicator 3H17 30 20 Centering of Brushes on Slip Rings 3H18 30 21 Wiring Schematic Electric Propeller Deicing System 3H18 30 22 Modular Brush Assembly Wear Check 3H20 30 23 Angle of Contact...

Page 493: ...witch 3L16 32 27 Gear Warning Switches Installation 3L16 32 28 Nose Gear Wear Limits 3L18 32 29 Main Gear Wear Limits 3L21 33 1 Logo Light Assembly Adjustments 4B17 34 1 Instrument Air System Installa...

Page 494: ...lancing 4115 61 1 Propeller Installation 4122 61 2 Typical Nicks and Removal Method 4123 61 3 Propeller Governor 4J3 61 4 Propeller Synchrophaser Installation Woodward Type I 4J5 61 5 Propeller Synchr...

Page 495: ...art No 18338 00 5H9 95 2 Fabricated Tail Stand 5H10 95 3 Protective Closures Installation 5H11 95 4 Fabricated Bellcrank Rigging Tool 5H12 95 5 Fabricated Aileron and Elevator Rigging Tool 5H 13 95 6...

Page 496: ...ed 2G21 2405 Specific Gravity Temperature Correction 2G22 2406 Capacity Ratings at Discharge Rates 2G23 2407 Electrolyte Freezing Points 2G23 2408 Circuit Load Chart 2H7 2601 Pressure Temperature Corr...

Page 497: ...ooting Pneumatic System Pressure Gauge 4E5 3903 Troubleshooting Engine Oil Pressure Gauge 4E5 3904 Troubleshooting Fuel Pressure Gauge 4E6 3905 Troubleshooting Air Temperature Gauge 4E9 3906 Troublesh...

Page 498: ...libration Data 5C21 7702 Digital Analog Torque Calibration Data 5C23 7703 Weston Kulite Torque Pressure Indicating System Tansducer Voltages 5C24 7901 Oil Pressure Gauge Calibration Data 5D17 9101 Lis...

Page 499: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3A24...

Page 500: ...CHAPTER FUEL 3B1...

Page 501: ...3B 19 28 15 02 Handling of Repair Materials 3B20 28 15 03 Repair Limitations of Fuel Cells 3B20 28 15 04 Repair Patch Heat Cure Method 3B21 28 15 05 Repair Patch Air Cure Method 3B23 28 15 06 Metal Fi...

Page 502: ...Filter 3C9 28 22 04 Assembly of Fuel Filter 3C9 28 22 05 Installation of Fuel Filter 3C9 28 23 00 Fuel Pumps 3C9 28 23 01 Removal of Submerged Fuel Pumps 3C9 11 82 28 23 02 Installation of Submerged F...

Page 503: ...stem is the crossfeed which is also mechanically operated from the fuel control panel This valve should always remain OFF except under single engine operation when crossfeed to the operating engine is...

Page 504: ...tion in inlet Trace lines and locate pressure surges side of pump obstruction Faulty pump Replace pump Low fuel pressure Fuel valve stuck Check valve No fuel in tanks Check and fill Filters dirty Clea...

Page 505: ...ly grounded transmitter installation 1 2 tank when tank and repair is full but will function normally on other tank No fuel pressure Shutoff valve off Turn on indication Fuel valve stuck Check valve N...

Page 506: ...7 CROSSFEED VALVE 28 SOLENOID VALVE 29 FIREWALL SHUTOFF VALVE 30 SOLENOID VALVE 31 CANISTER 32 CHECK VALVE 33 CHECK VALVE 34 SUBMERGED FUELI 38 PUMP 35 FUEL QUANTITY SENDERUNIT 36 VAPOR BLEED LINE 37...

Page 507: ...FUEL SHUTOFF RIGHT 7 SUBMERGED FUEL PUMPS RIGHT SEE NOTE 8 CHECK VALVE 9 CONTROL CABLE 10 HEATER FUEL LINE FITTING 11 CONTROL CABLE 12 VALVE ASSEMBLY FUEL CROSSFEED 13 SUBMERGED FUEL PUMPS LEFT SEE N...

Page 508: ...access plates from the top of the wing 4 Remove the lower wing root fairing and fuel cell drain fitting plates from the underside of the wing 5 By reaching through the nacelle opening remove the bolts...

Page 509: ...the cells to the skin brackets Push the cell down and work the nylon cord back through the cell hangers and rib bushings to the ends of the cell compartment 14 Remove the screws that attach the adapte...

Page 510: ...access opening in the wing top and secure to the inboard rib with the four bolts that attach each of the pumps 11 Connect the electrical wires to the submerged fuel pumps and install the check valves...

Page 511: ...BOLT ASSEMBLY 6 REQ 7 PLATE ATTACHMENT WING MAIN SPAR 8 SENDER 9 PLATE ATTACHMENT WING REAR SPAR 2 TORQUE BOLT 50 TO 70 INCH POUNDS 10 FITTING 11 WASHER TORQUE BOLTS 20TO 12 BOSS 14 LINE ASSEMBLY 5 BO...

Page 512: ...ASSEMBLY 14 LOOPATTACHMENT 1 SUBMERGED FUEL PUMP 15 LINER FUEL CELL 16 CHECK VALVE 17 KNOT AND WASHER 18 COVER FUEL CELLNDER 5 FUEL SENDER 19 DRAIN LINESKET 7 ACCESS COVER SCREW ASSEMBLY FLAPPER VALV...

Page 513: ...MBLY ACCESS 2 FUEL CELL 3 WING SKIN 4 KNOT AND WASHER 6 TIE KNOTS 6 RIB ASSEMBLY 7 LOOP ATTACHMENT 8 CORD 9 LINER ASSEMBLY 10 SNAP BUSHING 11 FUEL SENDER 12 GASKET Figure 28 6 Fuel Cell Installation O...

Page 514: ...RAFT T 1040 MAINTENANCE MANUAL STEP STEP STEP STEP STEP STEP STEP 1 2 3 4 5 6 7 Figure 28 7 Fuel Cell Tie Detail Figure 28 8 Installation of Fuel Valve Drain Plate 28 11 04 Page 28 12 3B15 Issued Marc...

Page 515: ...ells are to be cleaned inside and out with soap and warm water WARNING Usea vapor prooflightfor inspection NOTE To determine if fuel cell is repairable reach through the fuel cellaccess plate and take...

Page 516: ...defective cap to manufacturer for repair FUEL CELL COMPARTMENT 1 Thoroughly clear the cell compartment of all foreign material such as trimmings loose washers bolts or nuts 2 Round off any sharp edges...

Page 517: ...natural contours if possible while repairing Prevent contact with sharp edges corners dirty floors or other surfaces Repair area must be well ventilated Do not stack cells Inspect cavities and insure...

Page 518: ...roomtemperatureof approximately75 F For each 10 drop in temperatureadd 20 hours to cure time For instance if roomtemperaturereads65 F aircurefor 92 hoursinstead of 72hours The repair of GoodyearVithan...

Page 519: ...ch direction 3 Outside patches are to lap defect edges 25 to 50 inches larger than inside patches 4 Outside patches are to be applied and cured prior to applying an inside patch 5 Blisters between inn...

Page 520: ...xture thoroughly for five minutes NOTE Cement must be at a minimum of 70 F before mixing Keep awayfrom water and excessive heat 7 Brush one even coat of mixed repair cement on the cell wall around inj...

Page 521: ...s necessary to perform the repair Group II equipment will be furnished at additional cost if ordered by customer Foam Rubber Cloth Back Sheet 1 4 x 12 x 12 2 Paint Brush 1 inch wide 2 Aluminum plates...

Page 522: ...72 hours undisturbed at 75 F METAL FITTING SEALING SURFACES 1 Rub off roughness of affected area with a fine file or fine emery cloth Treat reworked area 2 Clean metal surface using a clean cloth dip...

Page 523: ...ither method may be used See Repair Patch Loose seams may be trimmed if minimum lap remains 4 Loose Fitting Flange Inside Buff edge of flange and contact surface under flange Apply 80C27 mixed repair...

Page 524: ...and preferred test REPAIR OF LEAKING NACELLE FUEL TANK The following procedure should be used for repairing leaks in the nacelle fuel tank The use of the specified material will allow the least amount...

Page 525: ...oating has been formed remove the excess solution by wiping with a clean water moistened cloth and wipe dry WARNING Do not allow alodine solution to come in contact with hands eyes or clothing 5 Lust...

Page 526: ...r application of the sealant QUICK DRAIN VALVE An optional quick drain valve is located in the wing root fairing It would take approximately 40 minutes to gravity drain a full tank containing 150 gall...

Page 527: ...ndthe mainvent line connectedto it Thisventwellis sealedfromthe fuel storage area in the tip tank exceptfor the float valve andrelieftube whichextendsto the forwardtopportion of the tank The float val...

Page 528: ...ned 7 Disconnect the fuel line from the aft end of the valve and control cable from the actuator arm on the valve 8 Disconnect the valve from the mounting bracket and unscrew and remove the valve from...

Page 529: ...the valve body Place the valve in the valve body so that the valve is allowed only 90 travel between stops 4 Lock the valve in the valve body by installing the snap ring on the valve 5 For the fuel sh...

Page 530: ...he clevis eitherway ifnecessarytoalignwiththe holeinthearm thensecurewithattachinghardware 5 Workthe particularcontrolseveraltimesto makesure the actuatorarm on the valvecontactsthe stop pinbeforethec...

Page 531: ...MANUAL 3 4 6 7 8 1 FUELLINE 2 HEADASSEMBLY 3 O RING 4 FIREWALL 5 FILTER ELEMENT 6 O RING 7 BOWLASSEMBLY 8 FUELDRAINLEVER 9 DRAINTUBE 10 DRAIN FILTER 11 CLAMP 10 9 Figure 28 13 Fuel Filter 28 22 02 Pa...

Page 532: ...fire wall fuel valve ON and depress the fuel filterbowl drain valve until a steady flow of fuel is noted Release handle and check for leaks where the filter bowl assembly screws into the head assembly...

Page 533: ...l Eitherpumpisremovedin thismanner INSTALLATIONOF SUBMERGEDFUEL PUMP Referto Figure28 14 1 Installationof either fuel pump is accomplishedby first installinga new gasket on the fuel pump mountingboss...

Page 534: ...ank A Removethefairingbetweenthetip tankandwing B Disconnect theelectricalleadsattheconnectors nexttothesensorunit C Checkthatthe tiptankis completelydrainedof fuel RefertoChapter12 DrainingFuelSystem...

Page 535: ...age and capacitance TESTING WARNING Use of a hand cranked megger or some other kinds of test equipment CAN CAUSE AN EXPLOSION if used on TANK UNITS OR THEIR WIRING HARNESS when in the presence of fuel...

Page 536: ...8808 Test Sensor Units or Gauge in aircraft or on bench for electrical leak age or capaci tance and cali bration or Test Set System Harness 89 108 2 Ragan Data Systems 3 Oval Drive P O Box 417 Central...

Page 537: ...KUNIT CAPACITANCE DRY Unit Location Main Inboards Main Outboards Nacelles Tip Tank Piper Part No 50946 04 550 578 50946 05 550 579 50946 02 550 576 50946 03 Tank Unit Model Capacitance pF PBA1020 1 12...

Page 538: ...QUANTITY INDICATOR When testing one side of a fuel quantity indicator the meter for the opposite side should be activated to approximately mid scale with a fixed capacitor of about 100 pF See Figure...

Page 539: ...A1020 1 PBA1020 3 MAIN TANK NACELLETANK PBA1020 2 AUX TANK PBA1021 TIP TANK IF INSTALLED PBA1021 TIP TANK IF INSTALLED PBA1020 2 AUX TANK NOTES 1 CONTINUITYOF HIGH IMPEDANCE SHIELD MUST BE MAINTAINED...

Page 540: ...SHOWN 3 UNDER TEST CONDITIONS BOXMUST BE INSULATED FROMGROUNDWITH GROUNDPOST CONNECTED TO SHIELD OF HIZCOAXTESTCABLE AND FLANGEOF SENSOR UNDERTEST 70 DIA Figure 28 15A Fabrication Of Test Fixture For...

Page 541: ...40 MAINTENANCE MANUAL CAPACITANCE TESTER 0 UNSH Figure 28 16 Alternate Indicator Bench Test Hookup COAX HIZ UNSHIELDEDLO Z Figure 28 16A Test Cables For Tank Unit Testing 28 43 02 Page 28 38 Issued Fe...

Page 542: ...n the capacitancetester Whenthe dial on the indicatorreads 700 pounds notethesereadings B Rotatetheindicator90 degreesclockwiseandrepeatStepA above againnotereadingsobtained C Rotatetheindicator90 deg...

Page 543: ...side NOTE The electrical system must supply power to the gauge to make these checks The gauge must read zero with unusable fuel in the tank and below zero when turned off 5 With the master switch ON...

Page 544: ...EGGER DANGER OF EXPLOSION See warning under paragraph titled Cleaning of Tank Units Trouble Cause Remedy Dead gauge does notcome up to zero pounds No dc power to gauge Correct loss of 24V dc to gauge...

Page 545: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL FUEL CONSUMEDTOTALIZER OPTIONAL Referto Chapter73 Indicating END 28 45 00 Page 28 42 Issued February 3 1986 3C22...

Page 546: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 3C23THRU 3D8 INTENTIONALLYLEFT BLANK 3C23...

Page 547: ...CHAPTER HYDRAULICPOWER 3D9...

Page 548: ...stem ConnectingTest Unit Disconnecting Test Unit Cycling Landing Gear Checking Landing Gear Cycle Time Checking Time Delay Valve Checking Handle Release to Neutral Checking Priority Valve Checking Mai...

Page 549: ...09 Hand Pump Suction Screen 3E18 29 15 10 Reservoir 3E18 29 15 11 Manifold Assembly 3E 19 29 15 12 Power Pack Handle Release Mechanism 3E20 29 15 13 Manifold Installation 3E20 29 15 14 Installation an...

Page 550: ...ic Pump 3F6 29 17 04 Disassembly of Hydraulic Pump 3F6 29 17 05 Cleaning Inspection Repair of Hydraulic Pump 3F8 29 17 06 Assembly of Hydraulic Pump 3F9 29 17 07 Installation of Hydraulic Pump 3F11 29...

Page 551: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLYLEFT BLANK 3D13...

Page 552: ...ition it is locked inplaceby the actionof thehandlereleasevalveat the powerpack actingagainst thereleasemechanismdetent The handlewillremaininthispositionuntilit is manuallyreleasedor until fluid pres...

Page 553: ...the hydraulic fluid the standpipe in the reservoir prevents the fluid level from dropping below the emergency quantity required for the operation of thesystem by means of the hand pump The engine driv...

Page 554: ...in this Chapter CHART 2901 TROUBLESHOOTING HYDRAULIC SYSTEM Trouble Cause Remedy Landing gear system fails to operate Selector lever dis connected Connect lever Selector lever out of adjustment Select...

Page 555: ...pump inoperative Cable line or other ob struction restricting the travel required to fully select gear up or down Replace line Repair or replace cylinder Check valve operation Check systemopera tion...

Page 556: ...r Malfunction of actuator locking mechanism Faulty limit switch Turn off power and hand pump doors open Note With power off sole noid valve shuttles to door open and the doors may be opened without se...

Page 557: ...Examine seals and cylinder bores for damage 7 When the hydraulic system is completely flushed and there is no further indication of contamination reconnect the previously disconnected fittings and rep...

Page 558: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL Figure 29 1 Schematic Diagram Hydraulic System 29 11 03 Page 29 07 Issued March 26 1982 3D20...

Page 559: ...ATIC SYSTEM 22 UPLOCK HOOK RIGHT MAIN PNEUMATIC 23 PNEUMATIC ACTUATING CYLINDER RIGHT MAIN GEAR 24 PNEUMATIC ACTUATOR FOR RELEASING UPLOCK HOOK 25 FILTER VENT 26 GEAR DOOR ACTUATING CYLINDER RIGHT MAI...

Page 560: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL Figure 29 2 Schematic of Power Pack Electrical System 29 11 03 Page29 09 Issued March 26 1982 3D22...

Page 561: ...cketlocated at the lower forwardcorner of the nose access panel opening and connect the pressurehose from the test unit Open the valveon the suctionport and by placingthe controllever inthe up positio...

Page 562: ...nd that the landing gear is down and locked 9 Check the indicator lights for proper operation 10 Remove the airplane fromjacks CHECKING LANDINGGEAR CYCLE TIME When the hydraulic system on the airplane...

Page 563: ...G CYLINDER RIGHT 4 DOORACTUATING CYLINDER LEFT 5 GEARACTUATING CYLINDER LEFT 6 FILTER LEFT PUMP 7 HYDRAULIC PUMP RIGHT 8 EMERGENCY HANDPUMP 9 HYDRAULIC PUMP LEFT 10 POWER PACKASSEMBLY 11 GEARACTUATING...

Page 564: ...ernal leakage is in the hydraulic system Check actuators for internal leakage Repair or replace actuators as required If actuators are not defective Power Pack internal leakage is indicated Repair or...

Page 565: ...o handle release operations 7 Sethydraulictestunitbypassvalve fullopen 8 Place landinggearselectorhandle inthefullupposition 9 Veryslowlyclosethebypassvalve untilthehandletripsbacktoneutral Readthegau...

Page 566: ...king Pressure Hand Pump Check Valve Cracking Pressure Landing Gear Position Release Time Delay Valve Hydraulic Fluid Required Weight Dry Power Pack Hydraulic Fluid Flow Rate Both Pumps Operating Reser...

Page 567: ...of the pilot s seat under the floor and operate emergency hand pump to open landing gear doors 2 Disconnect door open line upper fitting from main gear door cylinder and connect hydraulic test unit p...

Page 568: ...GEARDOWN 11 FITTING VENT 12 HOSE VENT 13 ACCESS OPENING 14 POWER PACK 16 BOLT 16 SAFETY WIRE 17 DRAIN 18 LINE GEAR UP 26 19 PANELWHEELWELL 2 20 BLOCK 21 LINE RETURN R ENGINE 22 LINE PRESSURE R ENGINE...

Page 569: ...rd baggage compartment NOTE All disconnect and removal work can be accomplished from the upper baggage compartment access or right access panel 2 Drain the Power Pack by removing the drain cap from th...

Page 570: ...Dry withfilteredcompressedair Todisassembletheunit proceedasfollows 1 Removewire nut reservoircover andO ring Coveris a snugfit on reservoir Usea soft malletand tapcoverlightlyto remove 2 Removedefle...

Page 571: ...ESHADEDPARTS POPPET 6 AND POPPET SEAT 7 ARE MATCHED PARTSANDMUST BE REPLACED AS ANASSEMBLY PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL Figure 29 5 HydraulicPower Pack 3E9 29 14 00 Page29 20 Issued March 2...

Page 572: ...UCTION 49 SNAP RING 50 FILTER HAND PUMP 51 HAND PUMP RELIEF VALVE 52 ADJUSTING SCREW 53 SPRING 54 STEM 55 BODY SECONDARY RELIEF VALVE 56 BALL 57 SEAT 58 O RING 59 CHECK VALVE TIME DELAY 60 SNAP RING 6...

Page 573: ...RAINFITTING 2 MAIN RELIEF VALVE 3 PRIORITY VALVE 4 HAND PUMPSUCTION FILTER 6 HAND PUMPRELIEF VALVE 6 TIMEDELAYCHECK VALVE 7 DOORVENTVALVE 8 STANDPIPE FILTER Figure 29 6 Location of Power Pack Componen...

Page 574: ...eeve NOTE Be sure that the end of the hook is not over 06 inches long and use the hook with care to prevent scratching the bore in the manifold The sleeve will be hard to withdraw due to O ringfrictio...

Page 575: ...EEVE TRANSFER VALVE 8 0 RING SLEEVE 9 DOORSELECTOR SPOOL 10 SPOOLDOORSELECTOR 11 DOORSOLENOID VALVEASSEMBLY 12 SOLENOID DOOR 13 0 RING SOLENOID 14 SPRING PLUNGER RETURN 15 PLUNGER 16 PIN 17 LANDING GE...

Page 576: ...125 incheslong and pullthe poppetseat up andout of the body Hook throughtheholesinthesideof theseat anduse carenottodamage theboreinthebody 5 Reassemblepoppetintopoppetseat Thepoppetandpoppetseatare...

Page 577: ...ons springsandplungers CAUTION Take care when removing snap rings cartridges are spring loaded LANDINGGEAR HANDLE RELEASEMECHANISM Referto Figure29 8 1 Removelockwire 2 Usinga punch drivetherollpinout...

Page 578: ...MAINTENANCE MANUAL 7 1 SWITCHCAM 2 PIN 3 GEAR 4 PIN 5 DETENT CAM 6 INPUT SHAFT 7 RETURN CAM 8 PIN 9 ARM 10 PIN 11 LOCKWIRE 12 INPUT ASSEMBLYSHAFT Figure 29 8 Power Pack Handle Release Mechanism Wiebel...

Page 579: ...s DOOR VENT VALVE Refer to Figure 29 5 1 Install the piston into the vent valve body 2 Lubricate and install the O ring on the retainer screw retainer into the valve body tighten and secure with wire...

Page 580: ...ief valve body and securewith adjusting screw The adjusting screwprovidesadjustmentfor themainreliefvalve Installflushat thistime HANDPUMP RELIEF VALVE Referto Figure29 5 I LubricateandinstallO ringin...

Page 581: ...of the manifold opposite the rack O ring could be caught and damaged and would have to be replaced by a new 0 ring 3 Check that thelanding gear selector spool slides freely 4 Inspect the door solenoid...

Page 582: ...3 Matethemanifoldtothe PowerPackbody usingcareto preventdamageto theO ringson the transfer sleeves NOTE When mating the manifold with the Power Pack body index the landing gear selector spool rack wit...

Page 583: ...A VIEW A PIN ARM Figure 29 9 Safetying Control Arm Wiebel 3 RETURNCAMIN HORIZONTALPOSITION 1 1 MANIFOLD 2 LANDING GEAR SELECTOR SPOOL RACK 3 INPUT SHAFT GEAR 4 INPUT SHAFT RETURN CAM 5 LANDING GEAR S...

Page 584: ...CLAMPS BATTERY PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL GEARUP GEAR DOWN MS3106A 145 2S PLUG MS3057A 6A CLAMP 0 WIRE 18 GAUGE HARNESSLENGTH 2 to 3 FT Figure29 11 PowerPackTestHarnessSchematic 29 15 14...

Page 585: ...e to the pressureinlet portof the PowerPack The 2500psi gaugeis to operateoff thepressureline 4 Connectthe suctionhoseto thesuctionportof thePowerPack 5 If a vent hose is part of the test unit connect...

Page 586: ...djust handle return cartridges in such a manner that their return plunger balls touch the surface of the input shaft return cam slightly CAUTION Remove drill or punch from rigging hole A 5 The detent...

Page 587: ...OR SOLENOID VALVE Refer to Figure 29 6 1 Remove the caps from the door open and door closed fittings on Power Pack 2 Connect a test harness to the electrical plug of the Power Pack and to power source...

Page 588: ...7 The hydraulicPowerPackis nowreadytobeinstalledinthe airplane HYDRAULICSYSTEMCOMPONENT SERVICING OPERATIONOF GEAR SELECTOR HANDLEMECHANISM RefertoFigure29 13 Operation of the gear selector handle mu...

Page 589: ...SY 6 LEVERASSY 7 CABLEASSY 8 BRACKETASSY 9 CLAMP 10 CONTROLARM 11 BRACKETASSY 12 PIN WASHER AND COTTERPIN 13 SOLENOID 14 MOUNTINGBLOCK 15 PANELASSY 16 LIGHTASSY 17 CABLEATTACHMENTPIN 18 TERMINAL Figur...

Page 590: ...tedto obtainthe neutralpositionin both thecontrol arm andselector handle 7 Recheckthat the handlewillleavethedetentat 3 1 2to 6 pounds REMOVALANDINSTALLATIONOF HYDRAULICLINES Removea damagedhydraulicl...

Page 591: ...995C20 safety wire and replace cowl 7 After engine has been operated check for leaks HYDRAULIC PUMP HYDRAULIC PUMP OPERATIONAL CHECK To determine the operable condition of each hydraulic pump the foll...

Page 592: ...ginecowls as required by releasingskin fastenersandseparatingthe two halves 2 Placea drippan under theengineto catchspillage 3 Disconnectthetwohydraulichosesfromtheendof thepumpandcapthemtopreventcont...

Page 593: ...SPRING 6 GASKET 7 DRIVE SIDE ASSEMBLY 8 LOCKNUT 9 O RING 10 CENTER PLATE ASSEMBLY 11 DOWELS 4 12 SCREW SQC HD CAP 13 REAR SIDE ASSEMBLY 14 STUD 15 O RING 16 DRIVE PIN 17 SECONDARY SHAFT 18 SECONDARY G...

Page 594: ...dipped in solvent Do not scrub any surface with a tool that will scratch surface WARNING Wear goggles rubber gloves and provide adequate ventilation when using trichlorethylene or cleaning solvents R...

Page 595: ...O ringsealon therearsideassembly 8 Lightlyoilgearteethwithhydraulicfluidbeforecompletingassembly 9 Matethe rearsideassemblywiththecenterplate usingcautionto alignthe driveandsecondaryshafts withthere...

Page 596: ...gears for evidence of chipped teethor cracks aroundthe bore Measure thegear O D which should be 1 1646 1 1644 Visually inspect thebearing bores for scratchesand or scoring Lap the surface to remove an...

Page 597: ...all to prevent the loss of fluid prior to the hookup of thehydraulic lines 3 Holding both lines at a level higher than the pump pour hydraulic fluid MIL H 5606 into the lines 4 Remove one cap at a tim...

Page 598: ...al 2 Disconnectthe hydraulicpressureandsuctionlinesfromthe forwardendof the pump 3 Removethepumpfromitsmountingbracketby removingattachmentbolts 4 Removethepumpfromtheairplane 5 Coverthepressureandsuc...

Page 599: ...SPRING 12 GT RING 13 PLUNGER 14 QUICKCLICKPIN 15 0 RING 16 GLAND 17 BACKUP 18 BACKUP 19 O RING 20 SCRAPER 21 BRACKET 22 QUICKCLICKPIN 23 LINK 24 QUICKCLICKPIN 25 SCREW 26 LEVER 27 GRIP 28 ROLLPIN 29 H...

Page 600: ...atethecompleteglandandslideitontotheplungerwiththerecessedendonthe outside 7 Lubricate the bore of the pump body and slide the plunger with the gland into the pump body 8 Install the scraper into the...

Page 601: ...mp relief valve has opened CAUTION It is very important that the hand pump be operated very slowly as pressure is being increased to bleed the hand pump relief valve If the hand pump is operated rapid...

Page 602: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 3F16THRU3F20 INTENTIONALLYLEFT BLANK 3F16...

Page 603: ...CHAPTER ICEAND RAIN PROTECTION 3F21...

Page 604: ...alofAirfoilDeiceBoots 3G8 30 15 40 Repairof AirfoilDeice Boots 3G9 30 15 01 ColdRepair 3G9 30 15 02 Vulcanized Repair 3G12 30 15 03 MaterialsforVulcanizedRepair 3G12 30 15 04 Definitionof Terms 3G13 3...

Page 605: ...3H5 2R 2 84 30 21 08 Preparation and Application of Sealer 3H6 30 21 09 Wrinkled Deicer 3H6 30 21 10 Electrical Check of Air Inlet Deicer 3H7 R 3 84 30 22 00 Adjustment of Air Inlet Ice Protection Sy...

Page 606: ...gs Replacement of Slip Rings Deicer Boots Resistance Check of Deicer Boots Replacement of Deicer Boots Removal of Deicer Preparation of Surface Prior to Installation of Deicer Application of Cement In...

Page 607: ...taking place As the air is cooled it is routed to a tee in the line where a water separator accumulator is mounted This separator removes any moisture from the air before it enters the pressure regula...

Page 608: ...owly Inflation time 6 seconds Lines partially blocked or not connected securely Deicer pump valve not functioning System pressure not being attained Deicer puncture Check fitting in deicer port for pr...

Page 609: ...HOOTING PNEUMATIC DEICERSYSTEM cont Trouble Cause Remedy Deicers deflate slowly Lines partially Inspect and blow out lines cont blocked Overboard line from control valve partially blocked Inspect and...

Page 610: ...ective 2 SolenoidValve Checksolenoidvalve Activatesystemswitchto ONposition Solenoidvalveshould be actuatedimmediatelyfor 6 seconds as evidencedby anaudible click It mayalsobepossibleto feel thesoleno...

Page 611: ...9 COAT THREADS OF BOLTS WITH FEL PRO C 5A HIGH TEMPERATURETHREAD COMPOUND AND TORQUE65 85 IN LBS 14 GYRO PRESSUREGAUGE 15 PNEUMATIC PRESSUREGAUGE OPTIONAL 22 16 VACUUM EJECTOR 17 DEICERSHUTTLE VALVE 1...

Page 612: ...n disconnectthe pneumaticsystem enginebleed air line at the engine and connect a hose from shop air to the pneumaticline with air regulated to 22 psig The system operatingpressureis 18psig Beforecheck...

Page 613: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL ALL Figure 30 2 Pneumatic Deicer Boots Operation 30 11 06 Page30 07 Issued March 26 1982 3G7...

Page 614: ...mentintheeventof failure REMOVALOF AIRFOIL DEICE BOOTS Theremovalof deicerbootsshouldbedonein a wellventilatedareato avoiddifficultyfromthefumesof the solvents Materialsrequiredto removethe bootsare T...

Page 615: ...ckets Thoroughly roll the patch with stitcher roller Part No 74 451 73 and allow to set for ten to fifteen minutes D Wipe the patch and surrounding area from the center outward with a cloth slightly d...

Page 616: ...onductive cement Small oval patch 1 1 4 x 2 1 2 in Medium oval patch 2 1 2 x 5 inch Large oval patch 5 x 10 in Patch 5 x 19 inch No 4 cement patching only Cement brush 1 2 in 1 8 in Steel stitcher Eme...

Page 617: ...er in length and width than the size of surface ply patch Apply one coat of cement Part No 74 451 11 to damaged area and one coat to patch Allow cement to set until tacky Roll the surface ply to the d...

Page 618: ...nof just where this divisionbetween repairable and unrepairable damage exists will of necessity depend upon the careful judgement of the inspectorandupontheexperienceandtrainingof theworkman MATERIALS...

Page 619: ...NOTE Do not apply A 56 B conductive cement in any area of any electrical transmitting or receiving equipment 8 Stitch to force fabrics or gum elements together with metal or rubber roller stitch from...

Page 620: ...fetycan for Toluolor MEK Takescreenand springoutof solventcansbeforefilling so thatall sedimentmayberemoved 10 Cementsshouldbeof such a consistencythat theycanbe appliedin a thinsmoothcoating If theya...

Page 621: ...fully examine for soundness If in a tube inflate to 25 psig SURFACE SCUFFS Repair as follows I Wash surface to be restored and apply one coat of conductive cement Allow to dry thoroughly Add another c...

Page 622: ...T T 1040 MAINTENANCE MANUAL Figure 30 3 Marking and Cutting Scuff Figure 30 4 Routing Scuff Figure 30 5 Buffing Edge of Repair Figure 30 6 Hole through Surface of Tube 30 15 08 Page 30 16 Issued March...

Page 623: ...ement 6 Mask off 1 16inch beyond repair Using mill knife or putty knife apply Neoprene putty filling cavity flush with surface Make sure cavity is completely filled Remove masking tape and cure for 15...

Page 624: ...MAINTENANCE MANUAL Figure 30 7 Routing toTube Fabric Figure 30 8 Cutting Surface of Tube Figure 30 9 Cementing Buffed Area and Patch Figure 30 10 Applying and Stitching Fabric 30 15 12 Page30 18 Issu...

Page 625: ...sprovisionsfor airconnections etc PREPARATIONOF LEADINGEDGES If the leadingedgesare painted removeall paintincludingzincchromateprimer 1 Withone inch 1 maskingtape maskoff leadingedgebootarea followin...

Page 626: ...FT T 1040 MAINTENANCE MANUAL Figure 30 11 Placing and Stitching Gum Figure 30 12 Removing Trapped Air Figure 30 13 Masking Repair Figure 30 14 Applying Neoprene Putty 30 16 01 Page 30 20 Issued March...

Page 627: ...orresponding air connection stem Tinnerman or other suitable non kink hose clamps should be used for this purpose Tighten each clamp with a pair of slip joint pliers but do not squeeze the clamp so ti...

Page 628: ...nts used for installation are flammable and their fumes slightly toxic Therefore all work should be done in a well ventilated area away from any sparks orflames Use of solvent resistant type gloves is...

Page 629: ...In cold weather wash the boots with the airplane inside a warm hangar if possible If the cleaning is to be done outdoors heat the soap and water solution before taking it out to the airplane If diffic...

Page 630: ...oot RESURFACING CONDUCTIVE CEMENT The following materials are required to remove and replace the old damaged coating 1 Fine grit sandpaper 2 Two inch paint brush 3 One inch masking tape 4 Conductive n...

Page 631: ...ate heating elements the parting strip located on the foremost area of the slip and two shedding areas located within the throat Each propeller boot also contains a heating element Selection of a cont...

Page 632: ...UTION Engine inlet lip deicers can be damaged if heated without the cooling effect ofpropeller slipstream Do not press ground test button for periods longer than 10 seconds with propeller speed below...

Page 633: ...long the edge of the recess in the fiberglass 3 Fill any seams or pockets in the fiberglass with EC 801 sealing compound then scuff sand the entire area lightly Remove the sanding dust with a compress...

Page 634: ...ZONE PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL ZONE VIEW A A STEP 1 STEP 2 STEP 3 STEP 4 Figure 30 15 Engine Air Inlet Lip Deicer Installation 30 21 05 Page30 28 Revised March 5 1984 3H4...

Page 635: ...the boot on a clean flat dry surface with the wire leads side up Clean this surface with Methylethyl Ketone MEK or toluol and allow to dry 2 Clean the fiberglass lip of the air inlet with MEK or toluo...

Page 636: ...ce 12 Apply masking tape around the edges of the inlet where the boot meets the fiberglass edges See Figure 30 15 View A A to prevent sealer fromcontacting any areas beyond the deicer bootedges 13 App...

Page 637: ...steps A Fabricate a Length Rigging Gauge per information given in Figure 30 16a and a Test Harness and Connector per Figure 30 16a B With the lower cowl removed from the airplane remove the actuator a...

Page 638: ...DDEICEDOOR 5 AFTDEICEDOOR 6 TURNINGVANE 7 UPPERSTOPANGLE 8 MECHANICAL STOPS WHEN KIT 765 156 INSTALLED 9 VANERESTRAINT TUBE ASSEMBLY NOTLESS THAN0 064 VIEWB B VANE RESTRAINT TUBE ASSEMBLY FORWARD I CL...

Page 639: ...6705 2 555 818 PINS AMP 66359 558 467 ACTUATOR ASSEMBLY 28V POWER SUPPLY OR TO MATE UATORASSEMBLY I SEE ETAIL A I 10 32 SCREW 10 WASHER 10 WING NUT 2 REQ 38 256 HOLE 7 00 3 8 DETAILA 14 0 MATERIAL WOO...

Page 640: ...the open and closed positions to assure its proper operation M In the DEICE OFF position ascertain that both doors stop electrically before the mechanical stop is contacted Also insure that the rear...

Page 641: ...onverter shaft B Temporarily connect the electrical connector to the wiper motor and operate the motor ending with the switch in the PARK position Disconnectthe electrical connector 2 Assemble the wip...

Page 642: ...AFT 13 BRACKET 14 MOUNTING BRACKET 15 EXTENSION LOCK 4 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL SEENOTE 7 8 1 12 9 2 15 11 10 3 AIRCRAFTWITH SERIAL NOS 31T 8275001 31T 8275002 31T 8275003 AIRCRAFTWITH...

Page 643: ...d collar by five inches Lock the adjustment cam 3 To adjust the wiper blade angle loosen the nut on the wiper blade attachment stud and rotate the blade until it is parallel with the windshield center...

Page 644: ...nsed temperature falls below a predetermined lower value Provision is made to prevent the shutdown of the parting strip heater in the event a temperature sensor lead becomes broken A system interlock...

Page 645: ...d one or more heating elements is faulty 2 If a failure is detected the annunciator could stay on for 45 seconds 90 seconds or continuously A fault indication of 45 seconds illumination indicates an o...

Page 646: ...ER 6 DEICEPOWER CONTROL RELAYS 7 CIRCUIT BREAKER PANEL 8 ENGINE CONTROL PANEL 9 RIGHT ENGINE DEICESWITCH 10 LEFT ENGINEDEICESWITCH 11 ENGINE DEICEGROUND TESTSWITCH SEESKETCH A 12 LEFT ANDRIGHTDEICEANN...

Page 647: ...kin Pike Dresher PA 19025 B If uneven wear is found or if wobble is noticed set up dial indicator as shown in Figure 30 19 to check alignment of slip rings to propeller shaft 5 Modular Brush Assemblie...

Page 648: ...CH LEFT PROP DEICER LEFT ENGINE DEICE RELAY RIGHT LIP LEFTICE PROTECTIONSW INLETLIP 30A PROP LIP 1 5A PWR CONTROL 5A LEFTGEAR SAFETYSWITCH NOTE FOR REFERENCE ONLY REFER TO CHAPTER 91 FORSCHEMATIC RIGH...

Page 649: ...dware and disconnecting the engine wire harness 2 Remove assembly screws and separate modules and spacer NOTE The part number of each module is etched into the surface of the plastic housing Replace w...

Page 650: ...ithin0 005 inch overall deviation from flat not to exceed 0 002 inch over a 4 inch arc If necessary undercut insulation between sliprings to a depth of 020 to 030 inch belowthe contactsurfaceof the sl...

Page 651: ...NYLONSPACER P N 2E1260 ON 2 ONLY 3 WIREMARKER B 2 ASSEMBLY C 3 ASSEMBLY Figure 30 24 Brush Module Assembly 3E2011 1 SPACER 2 BRUSHMODULEASSEMBLY 3E2011 2 3 BRUSHMODULEASSEMBLY 3E2011 3 4 SCREW MS2469...

Page 652: ...hort or open at the brush to slip ring contact disconnect harness at the timer and use low range ohmmeter to read resistance from each deicer circuit lead to ground it should read 1 58 to 1 64 If this...

Page 653: ...e deicer loosen enough of the deicer to grasp in the jaws of a vise grip pliers or similar tool 4 Apply a steady pull on the deicer to pull it off the propeller surface Continue using MEK or Toluol to...

Page 654: ...medistancefrom the hubfor rotationalbalance 3 Removethe patternand remove any paint in the markedoff area Clean down to bare metal Next cleanthe area thoroughlywithMEKor acetone Forfinal cleaning wipe...

Page 655: ...ss than 75 If the humidity is 75 to 90 allow two hours drying time Do not apply cement if the relative humidity is higher than 90 After allowing the proper amount of drying time apply a second even br...

Page 656: ...fterapplyingthesealer E Allow24 hourscementcuringtimebeforeturningup propeller Allow72hourscuringtimebefore operatingthe deicers Handlethepropellercarefullytopreventdamagetothedeicers 2 Propellerdeice...

Page 657: ...2 pt per six bl Cleaning Solvent MEK Methyl Ethyl Ketone or Acetone Cleaning Cloth any clean lint free cloth 1in Paint Brush 2 in Rubber Hand Roller 1 4 in Metal Hand Stitcher Scissors Turco 3 Turco...

Page 658: ...dry for 24 hoursbefore startingengine WRINKLEDDEICERS RefertoFigure30 29 If edgeof deiceris foundwrinkled orloose tryrecementin Use MEKor Toluolto loosenthebond foran additional 1 4 inch beyondthe loo...

Page 659: ...nvenient place 4 Reconnect any circuit that may have been disconnected or remove paper shims that might have been used for making the final electrical check INSTALLATION OF DEICER LEADS AND WIRE HARNE...

Page 660: ...TENANCE MANUAL WIREHARNESS PROPDEICER TIE STRAP MS3367 6 CONNECTOR Figure 30 30 Prop Deicer Wiring Harness Attachment SECTION A A DEICER DISTANCE OFFILLER APPLICATION BOTH SIDEOFDEICER SECTION B B Fig...

Page 661: ...ion light is used in conjunction with the pneumatic deicing system to aid the pilot in detecting the formation of ice on the left wing leading edge during night flying operations For removal and insta...

Page 662: ...CHAPTER LANDINGGEAR 3I8...

Page 663: ...Installation of Main Landing Gear 3124 32 12 04 Adjustment of Main Landing Gear 3J1 32 12 05 Alignment of Main Landing Gear 3J6 32 13 00 Main Gear Door Assembly 3J7 32 13 01 Removal of Main Gear Door...

Page 664: ...Operation and Leaks Installation of Gas Storage Bottles Removing Pressure from Lines After Activation of System Rigging Emergency Extension System Nose Gear Actuating Cylinder Removal of Nose Gear Act...

Page 665: ...Selector Handle Mechanism 3K13 32 35 03 High Altitude Gear Operation 3K13 32 40 00 WHEELS AND BRAKES 3K15 32 41 00 Main Wheel Assembly 3K15 32 41 01 Removal and Disassembly of Main Wheel 3K15 32 41 02...

Page 666: ...rake Master Cylinder 3L7 32 44 05 Installation of Brake Master Cylinder 3L7 32 45 00 Parking Brake Valve 3L7 32 45 01 Removal of Parking Brake Valve 3L7 32 45 02 Disassembly of Parking Brake Valve 3L7...

Page 667: ...2 01 32 62 02 32 62 03 POSITION AND WARNING cont Position cont Adjustment of Inboard Gear Door Ajar Switch Adjustment Landing Gear Safety Switch Adjustment of Nose Landing Gear Safety Propeller Revers...

Page 668: ...locked in either the up or down position and the green lights will show when each individual gear is down and locked There is no indication light when the gear is up and locked The red light will also...

Page 669: ...position Selector lever cannot be moved to the gear up posi tion while the LEFT main gear strutis com pressed or with thepower off Ascertain that the LEFT main gear strut is ex tended and that thepowe...

Page 670: ...r replace switch Nose gear fails to lock up when handle returns to neutral Main gear fails to lock up Increase the actuator stroke Relieve door pinch by lengthening door oper ating rods Adjust rod Act...

Page 671: ...ottle switches Adjust doors Replace defective switch Adjust throttle switches Replace switch Replace defective part Nose gear shimmies during fast taxi take off and landing Defective wiring Internal w...

Page 672: ...internal parts in strut Incorrect operating pressure Service strut with air and or fluid Replace defective parts Inflate tire to correct pressure Wheel out of alignment toe in or toe out Oleo cylinder...

Page 673: ...the oleo strut in accordance with instructions given in Oleo Struts Chapter 12 and remove the airplane from thejacks REPLACEMENT OF T RINGS ON LOWER BEARINGS Refer to Figure 32 6 1 Place synthetic sea...

Page 674: ...1 HOUSING OLEO 22 TUBE PISTON 23 BOLTASSEMBLY 24 FORK 25 PIN COTTER 26 NUT AXLE 27 BOLTASSEMBLY 28 PIN COTTER 29 BOLTASSEMBLY 30 BEARING UPLOCK 31 TORQUE LINK LOWER PIPERAIRCRAFT T 1040 MAINTENANCE MA...

Page 675: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL A A A 24 Figure 32 1 Main Gear Oleo Strut Assembly cont 32 11 01 Page32 08 Revised August4 1982 3121...

Page 676: ...e as those given for the nose gear oleo ASSEMBLY OF MAIN GEAR OLEO Refer to Figure 32 1 1 Ascertain that all parts are cleaned and inspected 2 To assemble and install the orifice tube insert the orifi...

Page 677: ...with washers that is holding the link on its pivot shaft Slide thelink from the pivot shaft H The pivot shaft may be removed by reaching through the pivot shaft bracket access hole removing the bolt...

Page 678: ...ainting of areas where paint has chipped or peeled and replacement of parts INSTALLATION OF MAIN LANDING GEAR Refer to Figure 32 2 NOTE When assembling any units lubricate bearings and friction surfac...

Page 679: ...side of the bushing install spacer washers to maintain a minimum amount of side play Secure bolt and safety 8 The downlock rod may be installed by bolting the sliding end of the rod to the downlock h...

Page 680: ...e Clearance between the stops should not exceed 0 020 of an inch If clearance exceeds 0 020 of an inch and pin is not worn and the link through travel is within limits then hook must be replaced 8 If...

Page 681: ...BLY 40 HINGE OUTBOARD DOOR 41 BEARING HINGE 42 DOOR OUTBOARD 43 BRACKET DOOR 44 ROD RETRACTION 45 HOSE BRAKE 46 PIN DOWNLOCK 47 CLEVISBOLT 48 BUSHING 49 WASHER 50 BOLT HOOKPIVOT 51 BOLT NAS1309 44D 52...

Page 682: ......

Page 683: ...e uplock hook use the following procedure A Disconnect the uplock operating rod from the hook B Retract thegear being careful to keep the rod clear of moving parts C As the uplock roller approaches th...

Page 684: ...wire will not go through the check hole in the rod ALIGNMENT OF MAIN LANDING GEAR The following steps should be completed prior to checking and or adjusting main wheel alignment 1 Ascertain that the...

Page 685: ...wheel in desired direction 5 Recheck the wheel alignment If the wheel alignment is correct safety the castellated nut with a new cotter pin If the misalignment still exists separate the torque links a...

Page 686: ...has been properly adjusted 2 Adjust outboard door rods to their maximum length and bolt them to the bosses on the gear housing Retract gear and observe the amount of gap Shorten rods by several turns...

Page 687: ...ube and release the retainer ring from annular slot at the bottom of theoleo housing 9 Pull the piston tube with component parts from the cylinder NOTE Prior to disassembling the upper bearing with re...

Page 688: ...LTASSEMBLY 22 TORQUE LINK LOWER 23 WASHER SPACER 24 BOLTASSEMBLYL 25 TORQUELINK UPPER 26 TUBE PISTON 27 SHIMMYDAMPENER 28 BOLTASSEMBLY 29 BOLTASSEMBLY 30 BOLTSAND SAFETY WIRE 31 BRACKET 32 BUSHING 33...

Page 689: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 14 Figure 32 5 Nose Gear Oleo StrutAssembly cont 32 21 02 Page32 22 Issued March 26 1982 3J11...

Page 690: ...TON SKETCH A SKETCHB INSTALLATION OF NON EXTRUSION RINGSINRODEND INSTALLATION OF NON EXTRUSION RINGSON PISTON SKETCHC SKETCHD CROSS SECTION OF INSTALLED T RINGASSEMBLY PROPERMATINGOF SCARF CUTON NON E...

Page 691: ...tion and secure assembly with retainer ring 6 At the top of the cylinder tighten the orifice tube bolt 7 Install the upper and lower torque links 8 Ascertain that the upper and lower oleo housing bush...

Page 692: ...and removing the rivets 13 The upper drag links attachment plates may be removed by holding the attachment nuts within the nose section and loosening the support bolts CLEANING INSPECTION AND REPAIR O...

Page 693: ...BOLT EYE 52 STOP STROKE 53 NUT LOCK 54 ROLLER UPLOCK 55 BOLTASSEMBLY 56 DUST BOOT 57 KEY LOCK 58 SWITCH PROPELLER REVERSE 59 RETRACTION ROD 60 IDLERLINK 61 ACTUATINGCYLINDER EMERGENCYGEAR EXTENSION 6...

Page 694: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 41 VIEW A VIEWB Figure 32 7 Nose Landing Gear Installation cont 32 22 02 Page 32 27 3J16 Revised November 15 1982...

Page 695: ...viduallyafter the support tube has been installed 4 The uplock hook with uplock spring may be installed as follows A Place the U end of the uplock spring over the back of the hook with the loops towar...

Page 696: ...against the retraction rod 9 Grasp the gear fork and rotate to determine that there are no gaps existing between the steering arm travel bushings and steering bellcrank which could cause the nose whee...

Page 697: ...plates and the lower link to the gear housing C Place the tool tube through the elongated hole in the tool plate and place the tube over and between the upper link attachment nuts D Swing the plate u...

Page 698: ...19 If gear fails to remain retracted after the cockpit handle returns to neutral it will be necessary to readjust one or all of the following until the gear will lock up A Increase the actuator strok...

Page 699: ...OB PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 21 EACH WAY 7 50 INCHTOTAL NEUTRAL TO FORWARD 3 87 IN NEUTRAL TOREAR 3 63 IN NEUTRAL ANGLE Figure 32 9 Rudder Pedals Neutral Angle CHALKLINE Figure 32 10 Al...

Page 700: ...ht and left travel mark on each side of the nose wheel a 40 degree angle line from centerline and wheel pivot point Turn wheel to maximum travel in both directions to check for allowable travel Should...

Page 701: ...SYSTEM A mechanically actuated pneumatic emergency extension system is incorporated into the landing gear systemof theT 1040 Pressurefor emergencyextensionof the gearsis providedby four sealed disposa...

Page 702: ...psig 7 Open the discharge valve on the test rig and insure that the particular landing gear extends properly and that there is no mechanical interference during the extension cycle NOTE The main gear...

Page 703: ...N DISCHARGE VALVE INDUSTRIAL NITROGEN BOTTLE 0 1500 PSI GAUGE BOTTLE DISCHARGER IN AIRCRAFT FABRICATEDTEST FITTING REFERTO CHAPTER 95 Figure 32 lOa Test Equipment Installation Emergency Gear Extension...

Page 704: ...extension systemis properlyriggedin accordancewith instructionsgiven in Adjustment of Main Landing Gear Usethe hydraulic test unit to supplyhydraulicpressureduringriggingoperations A With the airplane...

Page 705: ...ssarytopartiallyretractthegear totightenthe locknuts F Raise the gear until it is up and locked G Disconnect the emergency unlock actuator from the uplock hook and fully extend it Adjust the rod end u...

Page 706: ...LY OF NOSE GEAR ACTUATING CYLINDER WTC 2115 1 Refer to Figure 32 11 Lubricate all parts with hydraulic fluid per MIL H 5606 prior to assembly 1 Install GT ring on the head of the piston 2 Install back...

Page 707: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL WIEBEL TOOL COMPANY P N WTC 21 15 1 3 1 CYLINDER 2 GT RING 3 PISTON 4 O RING 13 5 BACK UP 14 6 END CAP 7 GT RING 15 I 8 SCRAPER STOP Issued March 26 1982...

Page 708: ...EBEL TOOL COMPANY P N WTC 2145 3 1 CYLINDER BODY 9 12 GT RING 10 3 PISTON 4 END CAP 6 BACK UP 11 7 GT RING 0 8 SCRAPER 9 NUT 10 KEY 11 ROD END 12 SAFETY WIRE Figure 32 12 Main Gear Actuating Cylinder...

Page 709: ...END CAP 65 15 CH POUNDS AND TORQUE LOCK 3 NUT 9 85 15 INCH POUNDS 1 CYLINDERBODY 2 GT RING 3 PISTON 4 END CAP 9 6 BACK UP 1 7 GT RING 8 SCRAPER 9 NUT 10 KEY 1 ROD END 12 SAFETYWIRE MS20995C32 13 FILTE...

Page 710: ...the bolt that secures the cylinder and the main gear uplock crank assembly 5 Remove the cylinder from wheel well DISASSEMBLY OF MAIN GEAR ACTUATING CYLINDERS WTC 2145 3 and WTC 2225 1 Refer to Figure...

Page 711: ...he actuating cylinder and cap the open line ends to prevent contamination 3 Disconnect the cylinder from the door and its mounting bracket 4 Remove the cylinder from the wheel well DISASSEMBLY OF GEAR...

Page 712: ...WIRE MS20995C20 6 PISTON 12 7 BALL 8 GT RING 9 0 RING 10 BACK UP 11 NUT 12 BARREL 13 NUT 14 BACK UP 15 O RING 16 RACE 17 PLUNGER 18 O RING 19 SPRING 20 SAFETYWIRE MS20995C20 21 FITTINGASSY 22 RETAINER...

Page 713: ...e all parts with oil per MIL H 5606 prior to assembly 1 Install O ring into groove of plunger 2 Install knurled nuts on barrel 3 Install back up rings and O rings into grooves of barrel 4 Install spri...

Page 714: ...does not rub the hoses Rotate the tire to check for possible High Spots on the tread 7 To bring the gear door back to the closed position turn the master switch ON place the gear selector switch in t...

Page 715: ...position with pin washer and cotter pin C Carefully thread the wires from the panel assembly through the hole provided in the plate assembly Position the panel assembly on the plate assembly Insert t...

Page 716: ...PLATEASSY 6 LEVERASSY 7 CABLEASSY BRACKETASSY 9 CLAMP 10 CONTROL ARM 11 BRACKETASSY 12 PIN WASHER AND COTTERPIN 13 SOLENOID 14 MOUNTINGBLOCK 15 PANEL ASSY 16 LIGHTASSY 17 CABLEATTACHMENTPIN 18 TERMIN...

Page 717: ...e main wheel and brake disc as an assembly it will be necessary to first remove the brake assembly Refer to Removal and Disassembly of Wheel Brake Assembly C Remove the snap ring that secures the axle...

Page 718: ...E DISC 4 SNAP RING 5 HUB CAP 6 BEARINGCONE 7 BEARINGCUP 8 GREASESEAL FELT 9 WASHER 10 AXLE SPACER 11 BOLTAND WASHER 12 SPUNED NUT 13 BOLT 14 VALVE ASSEMBLY USEDIF TUBELESSTIRESARE INSTALLED 15 O RING...

Page 719: ...be replaced B Small nicks or gouges in the castings should be blended out and polished with 400 grit sandpaper C Areas from which the protective coating has been removed or that show slight corrosion...

Page 720: ...y 8 Inspect the brake disc attachment bolts for cracks corrosion and thread damage Replace if necessary 9 To reassemble mount the brake disc in place install washers and bolts and torque to 150 inchpo...

Page 721: ...e axle 11 If the wheel and brake disc were removed as a unit proceed to step 15 Otherwise proceed as follows 12 Align the wheel assembly with the brake disc and install two bolts and washers finger ti...

Page 722: ...4 STEM VALVE 14 WEIGHT WHEEL BALANCING 5 GREASESEAL 15 SCREW 6 CONE BEARING 16 WHEELHALF OUTER 7 NUT 17 CUP BEARING 8 WASHER 18 NUT SELFLOCKING 9 BOLT 19 WEIGHT WHEEL BALANCING 10 WASHER FLAT 20 SCRE...

Page 723: ...s 6 The wheel bearing and seal can be removed by tapping out evenly from the inside with a brass drift Be careful not to damage the bearing cage INSPECTION OF NOSE WHEEL ASSEMBLY B F GOODRICH 1 Clean...

Page 724: ...acking groove on the wheel half 4 Install the tire and join the two wheel halves Apply a generous coat of thread compound MIL T5544 to threads of bolts faces of washers and bearing face of nuts Tighte...

Page 725: ...assemblies may be removed from each wheel half by first removing the snap rings that secure the grease seal retainers and then the retainers grease seals and bearing cones The bearing cups should be r...

Page 726: ...Remove the cylinder tie bolts and remove the back plate assembly 3 Remove the brake cylinder assembly from the torque plate the torque plate remains mounted to the axle 4 Remove the pressure plate ass...

Page 727: ...ATE 4 ANCHOR BOLT 5 BRAKECYLINDER 6 HOSE ASSEMBLY 7 0 RING 8 FRICTIONSPRING 9 PISTON 10 BOLTAND SEAL 2 EA 1 BOLTAND WASHER 2 EA 12 PISTON GUIDE 13 INSULATOR 14 LINING 15 SHIM 16 BACK PLATE 17 BLEEDERS...

Page 728: ...BODY ANCHOR BOLT HOLDING FIXTURE STEP A CYLINDER BODY ANCHOR BOLT HOLDING HOLDING FIXTURE FIXTURE STEP B STEP C PRESS CYLINDER BODY HOLDING FIXTURE STEP D Figure 32 20 Removal and Installation of Anc...

Page 729: ...before reinstallation 9 Inspect brake lining for edge chipping and surface deterioration 10 Replace brake linings which exceed the limits as shown in Figure 32 16 as follows NOTE If linings are change...

Page 730: ...ace piston in bore and rotate to seat drag ring and insure that piston and seal are in proper alignment C Tap the piston with a wooden or plastic mallet while alternately rotating If considerable effo...

Page 731: ...TUBE 3 RESERVOIR 4 MASTER CYLINDER RIGHT 6 MASTER CYLINDER LEFT 6 PARKING BRAKE VALVE 7 PARKING BRAKE HANDLE 8 FUSELAGE LINK 9 FLEXIBLEHOSE 10 GEAR LINK 11 BRAKE ASSEMBLY Figure 32 21 Brake Installati...

Page 732: ...2 Slide the packing gland O ring washer and spring from the piston rod 3 The piston valve assembly may be removed by first removing the self locking nut from the piston rod This will allow the piston...

Page 733: ...is pin 3 Connect the fluid lines to the cylinder PARKING BRAKE VALVE REMOVAL OF PARKING BRAKE VALVE 1 Disconnect the parking brake cable from the valve actuating arm 2 Disconnect the fluid lines from...

Page 734: ...cam into valve body and secure with spring bushing washer and self locking nut 3 Install ring on valve insert valve in hole of the out port install valve spring and secure with outlet fitting INSTALLA...

Page 735: ...VOIR CO PILOTS BRAKE MASTER CYLINDER LEFT RIGHT DUAL PARKING BRAKE VALVE OPEN CLEVELAND BRAKE SYSTEM CAP BLEED PORT PRESSURE GAUGE REGULATOR SHUT OFF BRAKE VALVE L BLEEDER FILL WITH SHOP AIR Figure 32...

Page 736: ...L ASSEMBLY Refer to Figure 32 25 1 Remove the left pilot s seat and the floor panel to the left of the control pedestal 2 Relieve the tension from the rudder control cables by loosening one of the cab...

Page 737: ...tube through the outer torque tube assembly installing the left pedals and left retainer collar 7 Insert the bolts through bolt retainer collars and tube do not install nut and determine number of sp...

Page 738: ...OLT CAP 34 BRAKE LINE SUPPORT 7 BOLT ASSEMBLY 21 BLOCK BEARING CHANNEL 8 ROLL PIN BOLT 22 BRACKET MOUNTING 35 TORQUE TUBE GUARD 9 CABLE END 23 PLATE 36 MACHINE SCREWSAND 10 BOLT ASSEMBLY 24 ROD NUTS 1...

Page 739: ...ng and extending gear several times ADJUSTMENT OF MAIN GEAR UP LIMIT SWITCH 1 Ascertain that the main landing gear uplock is properly adjusted 2 Retract gear fully and ascertain that the uplock roller...

Page 740: ...o that when the door is closed by hand a click can be heard approximately one inch before the door is completely closed CA UTION Avoid extreme outward adjustment that would cause the switch mounting t...

Page 741: ...and spacer block First remove the nut from each screw and allow the bracket of the other switch and spacer block to swing full forward by turning the adjustment screw counterclockwise Pull aft on the...

Page 742: ...WERLEVER RIGHT 3 ADJUSTMENT SCREW 4 MOUNTING BRACKET 5 ADJUSTMENT SCREW 6 MOUNTING BRACKET 7 HORN SWITCH 8 SPACER BLOCK 9 HORN SWITCH 10 SPACERBLOCK 11 TENSION SPRING 12 COIL SPRING 13 THROTTLELEVER A...

Page 743: ...anner in relation to the power levers for the adjustment of the gear up warning horn switches C Shut down the engines D Set the power lever at the locations marked With the adjustment screw on the swi...

Page 744: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 32 62 03 Page 32 77 3L18 Issued March 16 1982...

Page 745: ...6 NAS77 7 68 Upper Drag Brace 4375 0000 0035 Ream If Link Bushing Required 0010 Press Fit 7 NAS75 5 011 Upper Torque 4370 0000 0035 Line Ream Link Bushing 002 8 21831 04 Strut Cylinder 249 000 0020 P...

Page 746: ...0020 0015 Line Ream 16 NAS75 7 014 Upper Drag Brace 4375 0000 0035 Press Fit Link Bushing 0015 Line Ream 17 NAS77 7 38 Upper Drag Brace 4375 0000 0035 Press Fit Link Bushing 0015 18 20737 32 Idler Lin...

Page 747: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL Figure 32 29 Main Gear Wear Limits 32 62 03 Page 32 80 Issued March 26 1982 3L21...

Page 748: ...d 0015 Press Fit 5 NAS75 6 11 Link Bushing 4375 0000 0025 Ream If Required 0015 Press Fit 6 43256 2 Housing Bushing 3745 0000 0035 Line Ream OR 20737 40 0015 Press Fit 7 NAS75 7011 Link Bushing 4375 0...

Page 749: ...7 9 84 Fitting Assembly 565 0000 0025 Aft Bushing 0015 NAS77 18 88 1 1250 0000 0030 Forward 0015 19 NAS77 9 72 Bushing 5625 0000 0025 Press Fit 0010 20 NAS77 9 38 Bushing 6870 0000 0025 Press Fit 21 4...

Page 750: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3L24...

Page 751: ...MAINTENANCE MANUAL CARD 4 OF5 PA 31T3 T1040 PIPER AIRCRAFT CORPORATION 4A1 PART NUMBER 761765...

Page 752: ...roken down into Sub System Sections These sections are identified by the second element of the standardized numbering system The number 40 of the basic number series 32 40 00 is for the Wheels and Bra...

Page 753: ...RIAL NUMBERS 31T 8275001 TO 31T 8275025 INCL PA 31T T1040 1983 SERIAL NUMBERS 31T 8375001 TO 31T 8375005 INCL PA 31T T1040 1984 SERIAL NUMBERS 31T 8475001 AND UP 4A3 PIPER AIRCRAFT T 1040 MAINTENANCE...

Page 754: ...icated by a black vertical line along the left hand margin of the frame opposite revised added or deleted material Revision lines indicate only current revisions with changes and additions to or delet...

Page 755: ...h Electrothermal Propeller Deice Maintenance Manual P N 68 04 712 Latest Revision B F Goodrich Electrothermal Propeller Deice Installation and Removal Procedures P N 59 728 Latest Revision ENGINE PT6A...

Page 756: ...l Models Lear Siegler Inc Overhaul Manual Series 23048 P N 8013C P N 23700 P N 23202 PIPER PUBLICATIONS PARTS CATALOG INSPECTION MANUAL 100HOUR 761 761 Piper Aircraft Corporation 820 E Bald Eagle Stre...

Page 757: ...0497 Air Conditioning System Electronic Leak Detector Autopilot Avionics TIF Instruments 3661 N W 74th Street Miami Florida 33147 305 696 7100 Edo Corporation Avionics Division P O Box 610 Municipal...

Page 758: ...gines The B F Goodrich Company 6400 Goldsboro Road Suite 102 Bethesda Maryland 20034 301 229 5000 Leach Corporation 5915 Avalon Boulevard Los Angeles California 90003 213 232 8221 Narco Avionics Inc 2...

Page 759: ...Marmon Division 1214 Exposition Boulevard Los Angeles California 90064 213 774 3230 Aerosonic Corporation 1212 N Hercules Avenue Clearwater Florida 33515 813 461 3000 Landing Gear Hydraulic Actuators...

Page 760: ...nor Company Drake and Lemay Roads Fort Collins Colorado 80521 303 482 5811 Starter Generator Auxilec Incorporated One Willow Park Center Farmingdale New York 11735 516 694 1441 Lear Siegler Incorporat...

Page 761: ...NG AND TAXIING PARKING AND MOORING REQUIRED PLACARDS SERVICING STANDARD PRACTICES AIRFRAME ENVIRONMENTAL SYSTEM AUTOFLIGHT COMMUNICATIONS ELECTRICAL POWER EQUIPMENT FURNISHINGS FIRE PROTECTION FLIGHT...

Page 762: ...TRUCTURES DOORS FUSELAGE STABILIZERS WINDOWS WINGS PROPELLER STANDARD PRACTICES ENGINES POWER PLANT ENGINE TURBO PROP ENGINE FUEL SYSTEM IGNITION AIR ENGINE CONTROLS ENGINE INDICATING OIL SYSTEM START...

Page 763: ...r Doors IG11 12 9 Lubrication Chart Cabin Door Baggage Door Seats 1G12 12 10 Lubrication Chart Air Conditioner Quill Shaft 1G12 20 1 Torque Wrench Extension 1H1 20 2 Correct Method of Installing Rod E...

Page 764: ...4 Installing Pulley and Drive Plate Bearing 2E8 21 35 Installing Pulley and Drive Plate 2E8 21 36 Removing Coil Housing Retaining Ring 2E9 21 36a Positioning Sankyo Compressor Internal Parts 2E I 21 3...

Page 765: ...tion of Aileron Rigging Tool 2J 13 27 9a Wrapping Control Pedestal Aileron Trim Drum 2J 16 27 10 Trim Controls Installation 2J17 27 11 Aileron Control Travels and Cable Tension 2J 18 27 12 Safety Wiri...

Page 766: ...t Pump 3C10 28 15 Test Equipment Hookup 3C15 28 16 Alternate Indicator Bench Test Hookup 3C18 28 17 Fuel Gauge Adjustment 3C19 29 1 Schematic Diagram Hydraulic System 3D20 29 2 Schematic of Power Pack...

Page 767: ...e of Dial Indicator 3H17 30 20 Centering of Brushes on Slip Rings 3H18 30 21 Wiring Schematic Electric Propeller Deicing System 3H 18 30 22 Modular Brush Assembly Wear Check 3H20 30 23 Angle of Contac...

Page 768: ...itch 3L16 32 27 Gear Warning Switches Installation 3L16 32 28 Nose Gear Wear Limits 3L18 32 29 Main Gear Wear Limits 3L21 33 1 Logo Light Assembly Adjustments 4B17 34 1 Instrument Air System Installat...

Page 769: ...Balancing 4115 61 1 Propeller Installation 4122 61 2 Typical Nicks and Removal Method 4123 61 3 Propeller Governor 4J3 61 4 Propeller Synchrophaser Installation Woodward Type 1 4J5 61 5 Propeller Sync...

Page 770: ...rt No 18338 00 5H9 95 2 Fabricated Tail Stand 5H10 95 3 Protective Closures Installation 5HII 95 4 Fabricated Bellcrank Rigging Tool 5H12 95 5 Fabricated Aileron and Elevator Rigging Tool 5H13 95 6 Fa...

Page 771: ...cated 2G21 2405 Specific Gravity Temperature Correction 2G22 2406 Capacity Ratings at Discharge Rates 2G23 2407 Electrolyte Freezing Points 2G23 2408 Circuit Load Chart 2H7 2601 Pressure Temperature C...

Page 772: ...shooting Pneumatic System Pressure Gauge 4E5 3903 Troubleshooting Engine Oil Pressure Gauge 4E5 3904 Troubleshooting Fuel Pressure Gauge 4E6 3905 Troubleshooting Air Temperature Gauge 4E9 3906 Trouble...

Page 773: ...ibration Data 5C21 7702 Digital Analog Torque Calibration Data 5C23 7703 Weston Kulite Torque Pressure Indicating System Tansducer Voltages 5C24 7901 Oil Pressure Gauge Calibration Data 5D17 9101 List...

Page 774: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4A24...

Page 775: ...CHAPTER LIGHTS 4B1...

Page 776: ...ription of Operation 4B8 33 14 02 Removal of Annunciator Controller 4B8 33 14 03 Installation of Annunciator Controller 4B8 33 14 04 Annunciator Panel Lamp Replacement 4B9 33 14 05 Annunciator Panel O...

Page 777: ...33 42 03 Removal of Wing Tip Strobe Power Supply 4B15 33 42 04 Installation of Wing Tip Strobe Power Supply 4B15 33 42 05 Troubleshooting 4B15 1R 2 83 33 42 06 Removal and Installation of Wing Tip Rec...

Page 778: ...el lightsare illuminated to full intensity In the Dim mode lightingintensity may be controlled by any of four potentiometers located in the center of the overhead switchpanel The potenti meters contro...

Page 779: ...all E L lighting is inoperative check 24 V D C at junction point of RED wire on E L inverter and dimmer control box located on the electrical accessory shelf for 12V D C If any E L lighting is operati...

Page 780: ...72 028 472 028 758 418 472 049 472 769 472 052 472 028 753 477 753 478 761 208 453 886 472 029 761 214 762 003 472 061 GE387 GE313 GE327 GE464 A322 28 306 DA 27 GE327 GE327 GE327 AN3120 1047 GE4593 GE...

Page 781: ...TING SLIDE CONTROL One pot controls RIGHT PANEL LIGHTING SLIDE CONTROL One pot controls PLACARD LIGHTING One pot controls OPTIONAL AVIONICS RADIO LIGHTING 1 Ascertain all panel lighting refer above ar...

Page 782: ...than 28V D C essentialbus Three redundant display power master caution channels are provided and a minimumof two shall be connected also three redundant displaypower indicator channelsare provided an...

Page 783: ...resistive load of 128ohms across pin A and B of electrical harness connectors E 116and E217 Use a locally fabricated test box See Schematic Oil Temperature Right and Left 5 Ascertain the left fuel fl...

Page 784: ...located in the control pedestal between the indicator units The light bulbs may be replaced by first removing the aileron trim control knob by pushing out the roll pin that secures the knob Then remov...

Page 785: ...e plate into position to secure it in place OVERHEAD ENTRANCE LIGHT REMOVAL OF LAMP The removal of the headliner panel is necessary to replace the lamp 1 Remove the machine screws holding the circular...

Page 786: ...er 39 for location of electrical accessory shelf 2 With power OFF unplug connector E410 and loosen four 4 mounting screws INSTALLATION OF THE OPTIONAL CHIMES ASSEMBLY I Position chimes assembly on she...

Page 787: ...Refer to Figure 33 1 1 To remove either lamp from the landing light mounting plate remove the screws from the front of the lamp attachment plate and then remove the attachment plate from the lamp mou...

Page 788: ...obe lightis located inthe middle of the assembly The position and strobe lights are controlled by a separate switch located on the overhead panel There is a separate power supply for each wing strobe...

Page 789: ...pplied until the flashtube istriggeredby an externalpulse Thispulseis generated by a solid state timing circuit in the power supply When troubleshooting the strobe light system it must first be determ...

Page 790: ...4 Check tube socket assembly for shorts and opens A Disconnect the tube socket assembly of strobe light from the interconnecting cable B The following continuity checks can be made with an ohmmeter C...

Page 791: ...ght is positioned in the nacelle to illuminate the leading edge of the wing when the switch is activated in the cockpit SERVICING The only service required of this unit is the replacement of a burned...

Page 792: ...mp circuit breaker and controlled by a switch mounted on the overhead switch panel NOTES 1 Handling lamp with bare finger will deposit skin oil on lamp Remove before illumination of lamp by cleaning l...

Page 793: ...itch in off prior to securing light assembly or readjusting light asembly 6 Remove lens cover and tighten base locking clamp retainer screws and tighten yoke assembly reflector screws Reinstall lens c...

Page 794: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4B20...

Page 795: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4B21...

Page 796: ...CHAPTER NAVIGATION AND PITOT STATIC 4B22...

Page 797: ...r 4C6 34 20 00 ATTITUDE AND DIRECTION 4C7 34 21 00 Magnetic Compass 4C7 34 22 00 Directional Gyro Air Driven Electric 4C9 IR 2 83 34 22 01 Air Driven Directional Gyro 4C9 IR 2 83 34 22 02 Electric Dri...

Page 798: ...r systemconsists of two static ports one on each side of the fuselage These ports are inter connected as shown in Figure 34 1and the tubing is then routed forward along the top of the fuselageand down...

Page 799: ...RAFT NOT OPERATED IN CONTROLLED AIRSPACE UNDER IFR CONDITIONS SEE ADVISORY CIRCULAR AC 43 13 1A SECTION 4 OF CHAPTER 16 REFER TO PARTS CATALOG FOR TYPICAL SYSTEMROUTING 1 STATIC SOURCESELECTORVALVE 2...

Page 800: ...broken lacing and ties 8 Check instruments for evidence of overheating or contamination of equipment by foreign matter or water Dust dirt and lint contribute to overheating of equipment poor ventilati...

Page 801: ...he shock mounted instruments may be installed by the following procedure A Place the instrument in its proper panel cutout and secure with screws B Install the post light s and secure Do not overtight...

Page 802: ...Pointer oscillates Leaks in static lines Disconnect all instru ments connected to the static line Check individual instruments for leaks Reconnect instruments to static line and test installa tion for...

Page 803: ...tedtothe pointersthrough a mechanicallinkage Theinstrumentcaseisventedto the static air system and as static air pressure decreases the diaphragm expands causing the pointers to move through the mecha...

Page 804: ...eed indication depends on the differential pressure between pitot air pressure and static air pressure This instrument has the diaphragm vented to the pitot air source and the case is vented to the st...

Page 805: ...ON Circuit breaker popped Open circuit Reset Repair Excessive voltage drop between battery and pitot head Heating element burned out Check voltage at pitot head Replace pitot head NOTE When any conne...

Page 806: ...ion or broken jewel Remove excess compensation Replace or repair instrument Liquid leakage Loose bezel screws Replace or repair instrument Broken cover glass Defective sealing gaskets Replace or repai...

Page 807: ...The D G will agree onl with the Magnetic Heading from which it was set since all other subsequent Magnetic Compass Headings are subject to deviation Northerly Turning acceleration deceleration dip an...

Page 808: ...ading can be read mistakenly as precession Finally only after abnormal precession has been confirmed and the system installation proven good should the instrument be pulled for replacement or repair C...

Page 809: ...000 RPM thus producing the gyroscopic ability to remain rigid in the space The instrument case move freely about the spinning gyro rotor in three dimensions by the use of a gimbal assembly The result...

Page 810: ...nges after acceleration and deceleration The electric A H exhibits small errors in pitch and roll after roll out from a coordinated turn and also small pitch changes after acceleration or deceleration...

Page 811: ...tumbles in flight Pressure too high Defective instrument Instrument not set properly Instrument not level in panel Aircraft out of trim Normal if it does not exceed 1 16 inch Low pressure Dirty filte...

Page 812: ...chanically damped to slow or average minute yawand forcesto the human operators ability to interpret and respond to the displays The BALL portion of both instruments is free to roll within the incline...

Page 813: ...ance between rotor and rotor pivots Flat spot on ball Instrument not level in panel PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL CHART 3407 TROUBLESHOOTING GYRO HORIZON INDICATOR cont I rouble Cause Remed...

Page 814: ...9 Is electrical grounding in tact 10 Is circuit breaker correct or faulty 11 Are all electrical plugs and connections secure GYRO HANDLING AND SHIPPING The following information applies to all three...

Page 815: ...CHAPTER OXYGEN 4C17...

Page 816: ...ing of Face Masks 4DI 35 14 00 Components 4DI 35 14 01 Outlets 4D1 35 14 02 Removal of Outlets 4D1 35 14 03 Installation of Outlets 4D1 35 14 04 Oxygen Cylinder 4D2 35 14 05 Removal of Oxygen Cylinder...

Page 817: ...genoverboard through the dump outlet in the event of systemover pressurization High pressure oxygen is routed from the regulator to the pressure gaugewhilelow pressureoxygen is routed from the regulat...

Page 818: ...PPLY PRESSUREGAUGE 5 HIGH PRESSURELINE 6 OXYGEN CYLINDER 7 PRESSUREREGULATOR 8 FILLER VALVE Figure 35 1 Oxygen System Installation PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL NOTE THE NUMBER OF OXYGEN PL...

Page 819: ...ause Remedy Pressure indication normal but no oxygen flowing Oxygen cylinder regula tor assembly defective Replace regulator assembly Line obstruction Clean and purge lines No indication of pressure o...

Page 820: ...tems Teflon tape and Krytox 240AC 4 All oxygen system components must be handled with care to avoid damage 5 Prior to working on the oxygen system personnel must clean hands and tools Cleanliness is e...

Page 821: ...g 4 Any lines that are defective should be replaced with factory replacements 5 Clean all lines and fittings in accordance with Spec MIL 1 5585A PAR 3 11 Refer to Cleaning Oxygen System Components 6 R...

Page 822: ...with dry nitrogen 4 Flush withnaphtha blow unit cleanand dry withdry nitrogen Flushagain usinganti icingfluid anhydrous ethyl alcohol Rinse thoroughly with fresh water and purge dry with dry nitrogen...

Page 823: ...the rest of the mask with a very mild solution of soap and water 4 Rinse the mask thoroughly to remove all traces of soap 5 Make sure the sides of the breathing bag do not stick together while drying...

Page 824: ...mblyclamps that hold the cylinderin place 4 The cylindercan be removed by firstsliding it back to removethe retainingcable on aft mounted cylinder only 5 Remove the cylinder from the airplane using ca...

Page 825: ...LE TIES POSITION SLIT AWAY FROM WIRES ETC PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL 6 SKETCHB SKETCHA GROMMET CORRECT INCORRECT SKETCH D CLAMP WIRE BUNDLE EVERY TWO INCHES AT PASS OVERS Figure 35 2 Oxyg...

Page 826: ...LVE 1 Place the valve into position through the accessdoor and replace the three bolts and nuts 2 Tighten the three bolts and reconnect the tee fitting 3 Install previously removed panels PRESSURE GAU...

Page 827: ...DOT identification 2 The outlets should be checkedfor leakage both in the non usecondition and for leakagearound an inserted connector 3 The high pressure gauge may be checked for accuracy by compari...

Page 828: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK 4D6...

Page 829: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK 4D7...

Page 830: ...CHAPTER PNEUMATIC 4D8...

Page 831: ...val of Restrictor 4D13 36 11 09 Installation of Restrictor 4D13 36 11 10 Pressure Valves 4D14 36 11 11 Removal of Pressure Valves 4D14 36 11 12 Installation of Pressure Valves 4D14 36 11 13 Filter 4D1...

Page 832: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4D10...

Page 833: ...eice system pneumatic pressuregaugeand through a restrictorto the gyro instruments inlinefilterwheretheair is filteredbeforecontinuingonto the gyropressureregulatingvalve Atthe pressureregulatingvalve...

Page 834: ...S 1 BLEED AIR INTERCOOLER 2 BLEED AIR PORT 3 CHECK VALVE 4 ACCUMULATOR 5 PRESSUREREGULATOR 6 PRESSURERELIEFVALVE 7 RESTRICTOR 8 INLINE FILTER GYRO 9 PRESSUREREGULATINGVALVE GYRO 10 MANIFOLD 11 RESTRIC...

Page 835: ...out of the grommet in the fuselage skin 2 Attach accumulator mounting bracket to bulkhead with screws 3 Remove caps from lines 4 Attach tube to check valve Torque B nut 5 Attach tube to the aft side o...

Page 836: ...emove and cap lines to the pressure valve 3 Loosen nuts which retain the valve to the bulkhead 4 Remove valve INSTALLATION OF PRESSURE VALVES 1 Insert valve through hole in bulkhead 2 Tighten retainin...

Page 837: ...E REGULATOR Informationnot availableat this printing MANIFOLD The manifold is located on a bracket which is attached to the right pedestal cover and the left pedestal bulkhead REMOVAL OF MANIFOLD 1 Ga...

Page 838: ...al inlet fitting is positioned so that the drain hole drilled in one flat is positioned to the bottom of the cooler when installed Also ascertain that the insert part of this fitting is positioned wit...

Page 839: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL GRIDS 4D17 THRU 4D19 INTENTIONALLY LEFT BLANK 4D17...

Page 840: ...CHAPTER ELECTRIC ELECTRONIC PANELS AND MULTI PURPOSE PARTS 4D20...

Page 841: ...39 13 07 Removal and Replacement 4E4 39 13 08 Troubleshooting 4E5 39 13 09 Oil Pressure Gauge 4E5 39 13 10 General 4E5 39 13 11 Removal and Replacement 4E5 39 13 12 Troubleshooting 4E5 39 13 13 Fuel P...

Page 842: ...4E12 39 14 22 Removal and Replacement 4E12 39 14 23 Troubleshooting 4E12 39 14 24 Engine Torque Gauge 4E12 39 14 25 General 4E12 39 14 26 Removal and Replacement 4E12 39 14 27 Troubleshooting 4E13 39...

Page 843: ...4 Description of Operation 4E17 A 7 84 39 14 55 Annunciator Panel Adjustment Oil Temp 4E17 A 7 84 39 14 56 Removal and Replacement 4E19 39 14 57 Troubleshooting 4E 19 39 15 00 ELECTRICAL SWITCHES AND...

Page 844: ...tson the leftside infront ofthe pilot engineinstruments and electronicequipment inthe center Asecondset offlight instrumentsmav beinstalled in the right panel for use bythe copilot Theflightinstrument...

Page 845: ...electrical connector from the post light s G Disconnect the plumbing and or electricalconnector from the back of the instrument and identify each line to facilitate reinstallation Attach a dust cap or...

Page 846: ...MPERATURECONTROL PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 24 30 OXYGEN GAUGE 31 A C SWITCH 32 OXYGEN ON OFF KNOB 33 GROUND VENT FAN SWITCH 34 RECIRCULATINGAIR SWITCH 35 DEFROSTCONTROL 36 HEATER FAN SW...

Page 847: ...Electrical NOTE For information regardingthe sensitive altimeter rate of climb indicatorand magneticcompass referto Chapter34 Navigation and Pitot Static AIRSPEED INDICATOR GENERAL The airspeed indic...

Page 848: ...T 1040 MAINTENANCE MANUAL INDICATORS Remedy Check for leak and seal Replace instrument Replace instrument Find leak and correct Replace instrument Find leak and correct Re align pitot head Remove lin...

Page 849: ...te trouble and correct Faulty gauge Malfunc tioning pressure regulator Replace gauge Check oper ation of pressure regulator Low pressure indication High pressure indication Pressure regulator valve in...

Page 850: ...T 3904 TROUBLESHOOTING FUEL PRESSURE GAUGE WET DIRECT READING AND ELECTRIC Trouble Cause Remedy No fuel pressure indication Defectivefuel boost pump Check for fuel flow at firewallshutoff valve Defect...

Page 851: ...ck from the instrument panel 1 Remove the four screws which secure the clock to the panel 2 Reach up behind the instrument panel remove the clock from its position and move it to a more accessible loc...

Page 852: ...mal point annunciator overthe CLOCK legend and to place the display in the CLOCK mode B Pressthe SET button once The digitaldisplay willindicate the date Advanceto thedesired month by pressingthe DT A...

Page 853: ...istanceis indicated on the gauge in degreesFahrenheit and Centigrade REMOVALAND REPLACEMENT Refer to Removal and Installation of Instruments TROUBLESHOOTING CHART 3905 TROUBLESHOOTING AIR TEMPERATURE...

Page 854: ...c tions Check connections and tighten Defective instrument Replace instrument Meter does not indicate properly Meter out of calibration Replace with a calibrated meter FUEL QUANTITY GAUGE Dual GENERAL...

Page 855: ...transmitter is mounted on the firewall and monitors the fuel flow to the fuel control inlet The transmitter generates an electrical signal which is then transmitted to the fuel flow gauge REMOVAL AND...

Page 856: ...aulty electrical con nection Defective temperature bulb Improper calibration ad justment Remedy Check wiring to instrument and tighten connections Replace bulb Replace instrument ENGINE TORQUE GAUGE G...

Page 857: ...ly Propeller feedback ring or low pitch stop rods binding Engine torquemeter sys tem defective Calibrate pressure trans mitter Adjust Check feedback ring for run out and rods for free travel If engine...

Page 858: ...ans of a tachometer generato mounted on the reduction gear box case The tachometer generator provides an electric current directly pro portional to the speed of the propeller The gauge is calibrated i...

Page 859: ...OOTING Refer to Chart 3911 Troubleshooting Propeller Tachometer FLIGHT HOUR RECORDER GENERAL The flighthour recorder receives voltagefrom Batt Bus 2at all times However the ground circuit i through th...

Page 860: ...ster caution light a warning horn an individual indicator light cluster witha push to test s itch for theentire system and anelectronic annunciato controller whichis connected to sensors on the follow...

Page 861: ...r controller alsooffersdimmingof the warninglightsbyswitchingany lampgrounds offand on at a veryhighspeed no warninglamp flickeris visible butthedimmedlampsappear to belitby only10volts A fewannunciat...

Page 862: ...owly to illuminate the left oil temperature annunciator 9 Adjust the right channel in the same manner as the left channel in Step 8 NOTE In orderto properlycalibrateboth channels it may benecessaryto...

Page 863: ...ensor wiring point Faulty horn indicator light or reset switch Replace as necessary Point to point wiring Check circuit breaker and wiring connections NOTE 28 V D C Essential originates at Left Main B...

Page 864: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 3175 D B A C E Figure 39 3 Switch Panels 4E20 39 15 01 Page 39 21 Revised July 13 1984...

Page 865: ...ENTIAL BUS 4 LEFTDEICE BUS 5 RIGHTDEICE BUS 6 AVIONICS 1 BUS 7 AVIONICS 2 BUS 8 RIGHTMAIN BUS PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 3169 4 3 2 Figure 39 4 Circuit Breaker Control Panels 39 15 01 Pa...

Page 866: ...has two positions built into it for positioning the switch Be sure both upper and lower prongs on the switch body are in the same position on the clip 2 Install the switch in the electro luminescent p...

Page 867: ...faulty circuit breaker may be pulled from the assembly and replaced by a new one 4 Replace in reverse order all items removed in the preceding steps ELECTRICAL AND ELECTRONIC EQUIPMENT RACKS Refer to...

Page 868: ...RSEVOLTAGE ARRESTOR DIODE 12 ELECTROLUMINESCENTPANEL INVERTERS 8 13 AUTO IGNITION RELAY 14 STALL WARNING HEAT GROUND BLOWER MOTOR AND LIGHTING CIRCUITRELAY 15 COMBUSTION BLOWER MOTOR RELAY 16 WINDSHIE...

Page 869: ...CHAPTER STRUCTURES 4F1...

Page 870: ...REPAIRS Fiberglass Repairs Fiberglass Touch Up and Surface Repairs Fiberglass Fracture and Patch Repairs Thermoplastic Repairs Safety Walk Repair Surface Preparation for Liquid Safety Walk Compound P...

Page 871: ...facility be contacted WARNING No access holes are permitted in any control surfaces The use of patch platesfor repairs of all movable tail surfacesis prohibited The use of anyfiller material normally...

Page 872: ...25 025 032 032 040 040 9 10 11 12 13 14 2024 T3 2024 T3 321 STSTL 2024 T3 2024 00 2024 T3 THICKNESS 051 064 015 081 063 091 NOTE LEFT WINGSHOWN RIGHT OPPOSITE ANDNOTED MATERIAL OUTLINED IN DOTS USEDON...

Page 873: ...SITE ANDNOTED MATERIAL OUTLINED INDOTS USED ON RIGHT WING ONLY CIRCLED MATERIAL NUMBERS INDICATE LEFT WING ONLY Figure 51 1 Skin Thicknesses cont 51 00 01 Page 51 03 Revised November 151982 4F7 WING F...

Page 874: ...5 ELEVATOR 3171 I PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 314 2 2 2 NACELLE Figure 51 1 Skin Thicknesses cont 4F6 51 00 01 Page 51 04 Revised November 15 1982...

Page 875: ...HOLE REINFORCEMENT PLATE 17318 ACCESS HOLE COVER PLATE HOLE IN BOTTOM WING SKIN DIAMETER 4 16 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 166 PLATE ANS074 32 RIO Figure 51 2 Typical Access Plates and Pa...

Page 876: ...sswith the resin using a putty knifeor stick Add catalyst accordingto kit instruction to the resinand mix thoroughly A hypodermicneedlemaybeused to inject gel into smallcavities not requiring fibergla...

Page 877: ...be wet out on cellophane and applied as a sandwich Enough fiberglass cloth and mat reinforcements should be used to at least replace the amount of reinforcements removed in order to maintain the orig...

Page 878: ...d repairs to itemsmade of thermoplasticwhichareused throughout the airplane A list of material needed to perform these repairs is given along with suggested suppliersofthe material Commonsafetyprecaut...

Page 879: ...not to overheat the material Hold the nozzle of the gun about 1 4ofan inch away from the surface and apply heat with a circular motion until the area is sufficiently soft to remove the dirt particles...

Page 880: ...re 51 3 Surface Scratches Abrasions or Ground in Dirt Figure 51 4 Deep Scratches Shallow Nicks and Small Holes PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 671 0 51 12 00 Page 51 10 Issued March 26 1982 4...

Page 881: ...I 870 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THOROUGHLY MIX 825 Figure 51 5 Mixing of Epoxy Patching Compound Figure 51 6 Welding Repair Method 51 12 00 Page 51 11 Revised August 4 1982 4F13...

Page 882: ...ss is apparent or where thin walled sections are used the welding method is suggested J This welding method requires a hot air gun and ABS rods To weld the gun should be held to direct the flow of hot...

Page 883: ...pound to cure and insuringa good solid buildup of successivelayersas required 6 Stress Lines Refer to Figure 51 9 A Stresslinesproducea whitenedappearance in alocalizedarea and generallyemanatefromthe...

Page 884: ...I PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 831 PATCHING COMPOUND ABS Figure 51 8 Various Repairs 51 12 00 Page51 14 Revised August4 1982 4F16...

Page 885: ...INES I PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 827 Figure 51 9 Repair of Stress Lines PROFILE VIEWINDICATING DAMAGEDAREA Figure 51 10 Repair of Impacted Damage 51 12 00 Page 51 15 Revised August 4 19...

Page 886: ...slip included in Piper Part No 179872 APPLICATIONOF LIQUID SAFETYWALKCOMPOUND Liquid safetywalk compound shall beappliedin an area freeof moisturefor a period of 24hours mini mum after application Do...

Page 887: ...to dryfor 2 5 hoursmini mumprior to the applicationof the safety walk APPLICATIONOF PRESSURE SENSITIVESAFETYWALK Wipearea witha cleandry clothto insurethat no moistureremainson surface Donotapplywhens...

Page 888: ...CHAPTER DOORS 4F20...

Page 889: ...G3 52 12 02 Installation of Pilot Door 4G3 52 12 03 Weatherstrip Installation and Sealing Instructions of Pilot Door 4G3 52 12 04 Adjustment of Pilot Door 4G6 52 20 00 EMERGENCY EXIT 4G6 52 20 01 Emer...

Page 890: ...lation of Cargo Pod Door Removal and Disassembly of Cargo Pod Door Latching Mechanism Assembly and Installation of Door Latching Mechanism Cargo Pod Door Seal Installation 4G12 4G12 4G12 4G12 4G12 4G1...

Page 891: ...ame 3 Replace the upper door support assembly to the door REMOVAL OF CABIN ENTRANCE DOOR LOWER 1 Disconnect the support strap from the upper left door frame by unfastening the retaining hook 2 Disconn...

Page 892: ...ctuato assembly and removing the cotter pin and pin The handle and half of the actuator can now beremoved and further disassembled by removing two screws shim washers and plate from actuator Note the...

Page 893: ...NG 16 ACTUATORASSEMBLY 17 SPRING 18 ADJUSTING SCREW CABIN ENTRANCE 19 HOOK DOOR INSTALLATION 20 ROLLPIN 21 SHIM WASHERS 22 BOLTS 25 23 HANDLE INNER 24 DOORSNUBBER 25 LOWER DOOR 24 SUPPORT CABLE 26 UPP...

Page 894: ...between the door and frame Ascertain that there is at least 1 16 clearance between the shoulder on the latch pawl and the latch plate and that the pawl is completely engaged to the top of the latch pl...

Page 895: ...o obtain hinge center line location that will provide proper door fit 3 Attach the support assembly to the door WEATHERSTRIP INSTALLATION AND SEALING INSTRUCTIONS OF PILOT DOOR To obtain an acceptable...

Page 896: ...ter flows from the gap it is being funneled into 15 A person inside the aircraft can ascertain the sealing of the door NOTE It is not a recommended check to place large volumes of water over the aircr...

Page 897: ...11 MAIN LATCH ROD 12 BELLCRANK ASSY 13 INNERHANDLE ROD END 14 INNERHANDLE 15 OUTSIDE SKIN 16 CABLE FROM SKETCH A 17 CABLE FROM SKETCH B 18 BOTTOM LATCH 19 CLEVIS ROD END 20 HINGE PIN 21 BUSHING 22 SPR...

Page 898: ...SM ADJUSTMENT Adjustment is made by adjusting two turnbuckles which are located on either side of the emergency exit window frame 1 Remove the trim panel from between the first and second windows by r...

Page 899: ...oor and align hinges Insert new hinge pin and bend both ends 2 Attach door support assembly to door 3 Operate the door latch to determine the latch pins engage properly 4 Remove the clevis securing th...

Page 900: ...PORT 2 EYE BOLT 3 MAIN CABIN DOOR LATCH PLATE 4 CARGO DOOR LATCH 5 LINK 6 LATCHPIN GUIDE 7 LATCHPIN 8 ROD ASSEMBLY 9 SPACER 80 122 3 AS REQ TO INSUREPROPERLATCHING 10 SPRING RETAINERPLATE 11 SPRING Fi...

Page 901: ...in position with retainer plate 6 With installation complete operate the door latch to determine the latch pins move in and out of the pin guides smoothly WING LOCKER DOORS Refer to Figure 52 4 The on...

Page 902: ...racket by removing the cotter pin washers and pin 3 Removalprocedure for forward baggagedoor key lock assembly is as follows A Remove two screws from the outside of the door to disconnect the lock qui...

Page 903: ...E MANUAL 1034 7 1 NACELLE LOCKER 2 CATCH ASSEMBLY 3 BUCKLEASSEMBLY 4 BAGGAGE STRAP 5 DOOR SUPPORT 6 LOCKERDOOR 7 DOOR LATCH 8 LOCK ASSEMBLY Figure 52 4 Nacelle Wing Locker Latch Assembly 52 33 05 Page...

Page 904: ...tings located at the ends of the tube assembly 1 Remove the cotter pin washer and pin from the clevis and arm assemblies and loosen the locknuts between cleis and tube 2 With handle in the closed posi...

Page 905: ...2 5 1 To assemblethe door latching mechanism A Attach the latchplate to the pushrods with the pin washer and cotter pin B Attach the plungersto the pushrods with the pin washer and cotter pin C Slidet...

Page 906: ...0 2 1 PLUNGER 2 PLUNGER GUIDE 3 PUSHROD 4 SPRING 5 LATCHPLATEASSEMBLY 6 7 8 9 10 SPRING WASHER LATCH HANDLE PLATE LATCH STOP PLATE HANDLE ASSEMBLY PIN Figure 52 5 Cargo Pod Doors Latching Mechanism 4G...

Page 907: ...ected to the switch and mark them for positive identification when switch is reinstalled 3 Remove the two locknuts washers and bolts that secure the switch to the bracket on the door The switch can no...

Page 908: ...CHAPTER FUSELAGE 4G16...

Page 909: ...40 MAINTENANCE MANUAL CHAPTER 53 FUSELAGE TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION SUBJECT SUBJECT GRID NO EFFECTIVITY 53 00 00 53 00 01 GENERAL Description 4G 18 4G18 53 Cont Effec Page I Revise...

Page 910: ...tch at the lowersideis released the windowwillswingin and forward An emergencyexit is an integral part of the secondright windowand is jettisonable whenthe releasejust aft of the exit is pulled The ca...

Page 911: ...CHAPTER STABILIZERS 4G19...

Page 912: ...oval of Elevator 4H4 55 20 02 Installation of Elevator 4H4 55 20 03 Removal of Elevator Trim Tab 4H4 55 20 04 Installation of Elevator Trim Tab 4H4 55 20 05 Elevator Trim Tab Free Play 4H4 55 20 06 El...

Page 913: ...g must be accomplished in a draft free area and in a manner which allows unrestricted movement of the control surface BALANCING DEFINITIONS The following is a list of balancing definitions as used in...

Page 914: ...hat attach the elevator torque tube hinge bracket and rear spar 10 Pull the stabilizer directly away from the fuselage INSTALLATION OF HORIZONTALSTABILIZER Refer to Figure 55 1 1 Trial fit to ascertai...

Page 915: ...WASHER AN960 51 SEE NOTE TORQUE BOLT 100 140 IN LBS NOTE EITHER OF THE FOLLOWING COMBINATIONS MAY BEUSED 1 NUT RM52LH2935 054 RING 2935 05 OR 2 NUT H19300 5 WASHER K19301 5 BOLT AN3 7A NUT RM52LH2935...

Page 916: ...T 35 5 IN LBS BOLTAN174 14A WASHER AN960 416 2 REQ NUT MS20365 428C 298 BOLT AN3 4A 2 REQ TORQUEBOLT BOLTAN174 2 NUT AN310 4 WASHER AN960 416 COTTERPIN MS24665 132 2 REQ INB D BOLTAN174 13 WASHER AN96...

Page 917: ...OTE IN VIEW A TORQUE BOLT 100 140 IN LBS BOLT AN5 12A WASHER AN960 516 SEE NOTE IN VIEW A 2 REQ TORQUE BOLT 100 140 IN LBS 138 VIEW F BOLT AN5 1OA SEE NOTE IN VIEW A 2 REQ TORQUE BOLT 100 140 IN LBS B...

Page 918: ...A 2 REQ TORQUEBOLT 20 25 IN LBS 01 BOLT AN4 5 NUT AN310 4 COTTERPINMS24665 136 VIEW J 262 BOLT AN173 10 WASHER AN960 10 3 REQ NUT MS17825 3 COTTERPINMS24665 132 BOLTAN4 13A WASHER AN960 416 NUT MS2036...

Page 919: ...Y BEING CAREFUL NOT TO OVER TIGHTEN CAUSING BEARING PRE LOAD BOLTAN173 10 WASHER AN960 10 WASHER AN960 10L NUT MS17825 3 COTTERPINMS24665 172 TAB VIEW O C594 TOP SURFACEOF ELEVATOR BROKEN AWAY FOR CLA...

Page 920: ...rque 5 Install boltsattaching the torque tube bracketand elevator Ascertainthat the elevatorhalvesalign and tighten bolts use a protractor to check the angle between elevators 6 Insert the elevator tr...

Page 921: ...01 3 With the elevators assembled and mounted in the jig establish a horizontal reference mark which aligns with the trailing edge of the elevator when held in a level position chord line level Ascert...

Page 922: ...n pounds with 43 I pounds tension on elevator control spring with elevator in neutral position The following procedure will let you de termine the actual frictional value of the system 1 Attach a spri...

Page 923: ...ST WEIGHT ATTACHMENT POINT LOOSEN SCREW AND HANG WEIGHT OVER LEADING EDGE OF TIP KNIFE EDGES AT CENTERAND TWO OUTBOARD HINGE LOCATIONS BALANCE JIG MAIN BALANCE WEIGHT o 10 4 OZ TESTWEIGHT WEIGHT Figur...

Page 924: ...SCALE PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 310 TRAILING EDGE II I OUTBOARD I I I I TAB Figure 55 3 Friction Measurement 4H8 55 20 07 Page 55 12 Issued March 26 1982...

Page 925: ...ttach the front spar to the fuselage bulkhead 11 Removethe mounting bolts that attach the rear spar to the fuselage bulkhead 12 Pull the stabilizer directly up from the fuselage INSTALLATION OF VERTIC...

Page 926: ...oper cable tension as given in Chapter 27 with the rudder and control wheelscentered 5 Check rudder for proper operation Refer to Chapter 27 6 Install fuselage and cabin accesspanels REMOVAL OF RUDDER...

Page 927: ...duce a balanced condition Refer to Chart 5502 for the trim weight part number and the maximum amount allowed for the particular rudder assembly being balanced NOTE During this procedure the master tes...

Page 928: ...AL TAPETRIM TAB LEVELWITH RUDDER RUDDER BALANCE JIG MASTER TEST WT TESTWT ARM Figure 55 4 Rudder Balancing C445 TRIM WEIGHTS BALANCE WEIGHT Figure 55 5 Rudder Balance and Trim Weight Location 55 40 05...

Page 929: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4H13...

Page 930: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4H14...

Page 931: ...CHAPTER WINDOWS 4H15...

Page 932: ...val of Standard Windshield Installation of Standard Windshield Heated Windshield Removal of Heated Windshield Installation of Heated Windshield Windshield Repairs Repair of Windshield Window Sealant W...

Page 933: ...f PresstiteTape Number 163or equivalenton eachsideof windshield Foldexcess around edge No tape is needed between collar and windshield 3 Slide the windshieldinto place with the tape located under the...

Page 934: ...E 1 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 139 SECTIONA A 141 SEALANT MIL S 7502 OR MIL S 8802 CLASS B SIDE OF WINDSHIELD FOLD EXCESS AROUND EDGE 2 APPLY RTV SILICONE SEALER UNDER SCREWS AROUND PERI...

Page 935: ...ld Use only a non metallic window sealer 1 Apply Behr Manning Vinyl Sponge Tape I x 1 16 inches P N 542 or equivalent on the outside surface of the windshield around the outer edges 2 Apply masking ta...

Page 936: ...MIL S 8802 CLASS B 146 SEALANT MIL S 7502 OR MIL S 8802 CLASS B 145 SEALANT MIL S 7502 OR MIL S 8802 CLASS B VINYL SPONGE TAPE SECTIONA A SECTION B B VINYL SPONGE TAPE SECTION C C Figure 56 2 Windshi...

Page 937: ...eck is completed turn off switch WINDSHIELDREPAIRS REPAIR OF WINDSHIELD WINDOW SEALANT PPG Althoughthe materialusedinsealingthe windshieldisofahighquality exposuretothe naturalelements aircraft cleani...

Page 938: ...pportuni Delamination along the windshieldperiphery in the parting mediumarea is considerednormal A lo degree of adhesion is intended in this area A delamination area whichischaracterizedbyan irregula...

Page 939: ...WINDOW BULKHEAD TALLATION ST INS CR GE POINT OSS SECTION LOWERWINDOW INSTALLATION CROSS SECTION TYPICAL STORMWINDOW INSTALLATION LOWER EDGE CROSS SECTION STORM WINDOW GASKET MOULDING RIVET FRONT WIND...

Page 940: ...and press firmly into place CABIN SIDE WINDOWS REMOVALOF SIDE WINDOWS 1 Removethe screwsthat hold the trim molding around inside of the window 2 Removethe rivets that secure the window retainer moldi...

Page 941: ...CHAPTER WINGS 411...

Page 942: ...3 02 GENERAL AUXILIARY STRUCTURE Wing Tip Removalof Wing Tip Repair of Wing Tip Installation of Wing Tip ATTACH FITTINGS Wing Removal of Wing Installation of Wing FLIGHT SURFACES Aileron Removal of Ai...

Page 943: ...NG TIP The wing tip may be repaired in accordance withfiberglassrepair proceduresin the Structural Repairs portion of Chapter 51 INSTALLATION OF WING TIP 1 Attach the ground wire terminal to the wing...

Page 944: ...0 716 1 UNDER NUT 1 UNDER BOLTHEAD MS20365 720C PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 1024 1025 BOLTAN4 17A TORQUE TO 50 70 IN LBS WASHERAN960 416 WASHERAN960 416L NUTMS20365 428C 1 REQ L 1 REQ R S...

Page 945: ...1029 BOLTAN5 6A TORQUETO 100 140 IN LBS WASHER AN960 516 NUT MS20365 524C 5 REQ L 5 REQ R SHIM 44155 AS REQ AN7 15A TORQUE TO 450 500 INCHPOUNDS AN960 716 2 REQ MS20365 720C 18 REQ EEN BOLTAN5 12A TO...

Page 946: ...eft forward floor panel between the fuselageside trim panel and control pedestal NOTE To help facilitate reinstallation of control cables and fuel or hydraulic lines mark cable and line ends in some i...

Page 947: ...wingbutt willhaveto beremovedto allowthecableendto pass through B Disconnect the aileron balance cable and draw the cable from the fuselage Remove the cable pulley to allow cable to be removed C Remo...

Page 948: ...s cables etc to follow INSTALLATION OF WING Refer to Figure 57 1 1 Ascertain that the fuselage is positioned solidly on a support cradle 2 Place the wing in position for installation with the spar end...

Page 949: ...g and Adjustment of Aileron Chapter 27 and safety turnbuckles 21 If the left wing is being installed the following items pertain to the installation of the left wing only A Draw the left balance cable...

Page 950: ...alance weight 6 If the aileron balances with the master test eight installed it is at the minimum static balance limit and is satisfactory 7 If the aileron is leading edge heavy with the master test w...

Page 951: ...alance Weight Right 4 75 Pounds Left 3 9 Trim Weight Part Number 54395 2 Maximum Number of Trim Weihts Allowed Per Side 4 Maximum Allowable Balance Weihts Right 5 48 and Trim Weights Pounds Per Side L...

Page 952: ...nds Left 1 431lbs Inboard 6 00 lbs Not Allowed Trim Weight Part Number Maximum Number of Trim Weights Allowed Per Side Maximum Allowable Balance Weights and Trim Weights Pounds Per Side Not Allowed Ri...

Page 953: ...RAFT T 1040 MAINTENANCE MANUAL 1022 A 1021 SECTIONA A 117 WASHER3512 20 03 0511 16REQ OMITONCTR TRACKASSY WASHER40559 43 8 REQ OUTBD ASSY WASHER40559 42 16 REQ INBD CTR ASSY Figure 57 4 Aileron and Fl...

Page 954: ...EQ SKETCH B SKETCHC BOLT AN4 15 WASHER AN960 416 NUT AN3104 COTTER PIN MS24665 134 2 REQ TORQUE BOLTTO 38 IN LBS INCLUDES 18 IN LBS AVERAGE FRICTION DRAG TORQUE BOLT WASHE NG 41413 5 SKETCHE SKETCHD S...

Page 955: ...e tab back and inboard enough to remove the outboard hinge pin from its bushing Remove the tab INSTALLATION OF AILERON TRIM TAB Refer to Figure 57 4 1 Insert the tab control rod through the aileron an...

Page 956: ...the flap 4 Remove the upper roller assemblies from the flap brackets 5 Remove the lower roller assemblies and remove flap INSTALLATION OF FLAP Refer to Figure 57 4 1 Put the flap in position and inst...

Page 957: ...CHAPTER PROPELLER 4117...

Page 958: ...nor 4J2 61 22 01 Removal 4J2 61 22 02 Installation 4J2 61 22 03 OverspeedGovernor Operational Checks 4J2 61 23 00 Propeller Synchrophaser Woodward Type I 4J3 61 23 01 Description 4J3 61 23 02 Function...

Page 959: ...or Magnetic Phase Pickup Removal Installation and Adjustment Propeller Synchrophaser Woodward Type II Description Functional Test Troubleshooting With Minimum Field Equipment Ground Check Flight Check...

Page 960: ...mo e the spinner by removing the attachment screws that secure the spinner to the spinner bulkhead 2 Remove the engine cowling Refer to Chapter 71 3 Remove the deicer brush block assembly Use caution...

Page 961: ...h zerk fittings Remove one of two fittings for each propeller blade alternate the next time Apply grease through the zerk fitting until fresh greaseappears at the hole of the fitting removed Care shou...

Page 962: ...W STOP RODS 6 SPRING REVERSERETURN 7 SLIP RING ASSEMBLY DEICER 8 O RING 9 ENGINE MOUNTING FLANGE 10 BOLT 11 SPINNER BULKHEAD 12 FEEDBACK RING 13 REVERSINGLEVER 14 CARBON BLOCK ASSEMBLY 15 BRUSH BLOCKA...

Page 963: ...ance Torque the jam nuts at the feedback ring to 12 foot pounds Torque the nut on the front of the low stop rods to 22 foot pounds 8 Check the Beta valve Rigging 9 Perform an engine ground check and c...

Page 964: ...d by Hartzell CONTROLLING PROPELLER CONSTANT SPEED GOVERNOR REMOVAL 1 Remove the upper engine cowling per Chapter 71 2 Disconnect the electrical connections from the governor 3 Disconnect the prop pit...

Page 965: ...pressure tube at the governor connection and blank off nipple and pneumatic line with suitable caps 2 Perform the pre start check 3 Start theengine and allowit to warmup in the idle setting until nor...

Page 966: ...EMOVAL 1 Remove the engine cowling 2 Disconnect the electrical leads from the overspeed governor 3 Remove the nuts and washers securing the overspeed governor to the reduction gearbox and withdraw the...

Page 967: ...n the left engine propeller governor control thus maintaining the same propeller RPM as the master right propeller governor within a limited range Normal governor operation is unchanged but the synchr...

Page 968: ...ust be recentered in the followingmanner 1 Turn the systemswitch OFF 2 Manually synchronizethe engines 3 Turn the systemswitch ON If the systemdoes not operate properly perform the ground check listed...

Page 969: ...NOR LEFT 3 OVERSPEEDGOVERNOR RIGHT 4 PROPELLERCONSTANT SPEEDGOVERNOR RIGHT 5 CONTROLBOX 6 CIRCUITBREAKER 7 SWITCH 8 ACTUATOR 9 CONNECTOR 10 CONNECTOR 11 CONNECTOR 12 CONNECTOR 13 MAGNETIC PHASE PICKUP...

Page 970: ...ctuator per Chart 6103 5 4 3 13 to 17 ohms 6 5 to 8 5 ohms 13 to 17 ohms 6 5 to 8 5 ohms 13 to 17 ohms 6 5 to 8 5 ohms 3 1 STEP NO S 7 11 Test for Defective Pickup STEP NO S 12 13 Test Aircraft Wiring...

Page 971: ...Zero the ohmmeter and read on the XI or X10 scale NOTE If another accessory uses the same circuit protector turn this accessory off before starting tests The control box must be un plugged for these...

Page 972: ...for the master engine synchronizer pickup voltage These values should be between 85 volt minimum and 4 volt maximum for the synchronizer pickup These are RMS voltages as read on a 5000 ohm volt AC vol...

Page 973: ...TENANCEMANUAL EL1400 PROP SYNC CONTROL ASSY PROP SYNC SWITCH E334 CONN E04 CONN REFERTO SYNCHROPHASER SCHEMATIC CHAPTER91 Figure 61 5 Propeller Synchrophaser Diagram Woodward Type I 61 23 05 Page61 14...

Page 974: ...the rod end assembly paying particular attention to the bearing NOTE Rod end trimmers are lubricated witha baked on dry Molykote DO NOT OIL Engine oil should be kept clean Dirty engine oil will deposi...

Page 975: ...rimmer to one end of its travel Now move the cockpit propeller control through its complete range and observe the governor speed adjustment lever to be certain it hits both maxi mum and minimum RPM st...

Page 976: ...left propeller control lever to its aft stop push hard as this is inafriction range The stop on the governor must be contacted 7 Drive the synchronizer flex shaft to extend the trimmer to 437 of an i...

Page 977: ...verfrom the actuator and cleanthe internalparts such as micro switchesand electrical connections etc Apply Alpha Molykote G to the spiral groove of the switch actuating discat the end of the motor CON...

Page 978: ...is allows partially checking the control box without running the engines NOTE Use of any Woodward test equipment with the Woodward synchrophasersystem willrequirethe useof a Jones plug adapter Usethe1...

Page 979: ...edy MAGNETIC PHASE PICKUP REMOVAL INSTALLATION AND ADJUSTMENT 1 Remove the engine cowling Refer to Chapter 71 2 Disconnect electrical wiring from the magnetic pickup 3 Remove the safety wire from the...

Page 980: ...control box Excessive torque required to trim the governor in one direction this assumes the governor and propeller are equally responsive in each direction Determine the malfunction with wiring check...

Page 981: ...6 ft Vinyl coveredplastic insulated cable Belden types 8448 8 22 stranded wires GROMMET 1 5 8 O D x 3 8 I D black rubber grommet PLUG 1 Cinch Jones8 connector plug P N P 308 CCT SOCKET 1 Cinch Jones8...

Page 982: ...l box Mechanically misrigged Defective centering mechanism Switch arm bent Defective centering switches Rod end flexible shaft or actuator mechanically bound up Improper rigging Trying to synchrophase...

Page 983: ...spikes Repair offending electrical from other electrical accessory accessory Excessive mechanical Correct mechanical binding friction Synchrophaser operates Excessive mechanical Decrease torque requir...

Page 984: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL GRIDS 4J20 THRU 4K4 INTENTIONALLY LEFT BLANK 4J20...

Page 985: ...CHAPTER STANDARDPRACTICES ENGINES 4K5...

Page 986: ...MAINTENANCE MANUAL CHAPTER 70 STANDARD PRACTICES ENGINE TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO SUBJECT EFFECTIVITY 70 00 00 STANDARD PRACTICES ENGINE 4K7 70 Cont Effec Page 1 Is...

Page 987: ...the nut and unlessotherwisespecified bendoneendof the pin back over the stud or bolt andthe other enddown flat against thenut Useonlycorrosionresistantsteellockwireand or cotter pins Bushingplugs sha...

Page 988: ...CHAPTER POWER PLANT 4K8...

Page 989: ...1 30 01 GENERAL Description and Operation Troubleshooting Engine Removal Engine Buildup Engine Installation Engine Depreservation Engine Motoring Run Engine Ground Check and Safety Precautions COWLING...

Page 990: ...drives the compressor in the gas generator sectionand the second drives the propeller shaft through a reduction gearbox The engine lubricating system is a pressure type with the main oil pump located...

Page 991: ...esare completelyenclosedby cowlingsconsisting of an upper and lowersection of cantilever construction attached at the firewall A hingeddoor on the upper cowlsallowsaccessto theoilfillerneckand quantit...

Page 992: ...p Check for flow from FCU outlet tube to starting flow control while motoring engine If no flow remove FCU check bypass valve by applying 5 psi max to bypass re turn port and check for air leakage fro...

Page 993: ...orrectly Adjust linkage Defective fuel control unit Replace fuel control unit Engine does not develop full power Faulty engine instru mentation Check instrument system Replace or recalibrate as necess...

Page 994: ...OOTING ENGI Cause Propeller out of balance Compressor or compressor turbine disc out of balance NE cont Remedy Replace propeller Return disc to an overhaul facility Refer to Engine Maintenance Manual...

Page 995: ...on when working with the fire extinguisher system Accidental discharge may cause bodily injury 9 Remove the fire extinguisher system Refer to Chapter 26 10 Disconnect and cap oil cooler lines at engin...

Page 996: ...AIN 20 OIL BREATHER 6 ENGINE MOUNT ASSEMBLY 21 OIL PRESSURE LINE 9 OIL DRAIN 22 HYDR 10 START CONTROL DRAIN 23 FUEL 11 FUEL CONTROL DRAIN 24 PROPELLER CONTROL 12 SOLENOID VALVE 25 STAR 522 23 THER LIN...

Page 997: ...TS 160 TO 190 IN LBS PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL RIGHT SIDE VIEW 3154 LEFTSIDE VIEW TORQUE ALL MOUNT ATTACHMENTS 160TO 190 IN LBS Figure 71 1 Powerplant Installation cont 71 00 03 Page 71...

Page 998: ...ION Referto the Pratt and WhitneyEngineMaintenanceManual Part No 3030442before attempting to remove a new enginefrom the shippingcontainer ENGINE INSTALLATION The installationof eitherengineisbasicall...

Page 999: ...nce Manual Part No 3030442 14 Check for fuel and oil leaks and security of the engine components ENGINE DEPRESERVATION After completionof a newengine installation and beforethe firstengine start the f...

Page 1000: ...aveignition switch OFF 7 Operate the starter for 10seconds CAUTION Do not exceedstarter time limits 30secondsON I minuteOFF 30 seconds ON I minuteOFF 30 secondsON 30 minutesOFF 8 Releaseengine starter...

Page 1001: ...ock pitch test switches while continuing to move the power levers toward reverse The prop should not go into reverse and the lights should blink C Continue to move the power levers toward reverse unti...

Page 1002: ...3 STRIPASSEMBLY FORWARD 4 STRIPASSEMBLY AFT 5 LOUVREASSEMBLY 6 UPPER COWL 7 INTER COOLERINLET 8 STARTER GENERATORCOOLING DUCT 9 ACCESS PLATE FUELFILTER 10 ACCESS DOOR WASH RING 11 OIL COOLER AIR INLET...

Page 1003: ...ing pro cedures listed in Fiberglass Repairs Chapter 51 INSTALLATION OF COWLING Refer to Figure 71 2 The procedure for installing the cowl is the same for either engine 1 Position and support the lowe...

Page 1004: ...bly 5 Install the mount assemblyin reverseorder of removal Torque the pad mounting specialboltsto 225 to 300 inch poundsand safetywith MS20995 C41safety wire 6 Torque the mount bolt to the specificati...

Page 1005: ...CHAPTER ENGINE TURBO PROP 4L1...

Page 1006: ...CRAFT T 1040 MAINTENANCE MANUAL CHAPTER72 ENGINE TURBO PROP TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION SUBJECT SUBJECT GRID NO EFFECTIVITY 72 00 00 GENERAL 4L3 72 Cont Effec Page 1 Issued March 26...

Page 1007: ...athering reversingtype Refer to Chapter 61 The engine lubricating systemis covered in Chapter 79 The engine fuelcontrol systemis covered in Chapter 73 The engine ignitionsystem is in Chapter 74 For En...

Page 1008: ...CHAPTER ENGINE FUEL SYSTEM 4L4...

Page 1009: ...4L13 73 21 02 Preparation for Shipping 4L14 73 21 03 Preparation of Fuel Control Unit for Service OFF Engine 4L 14 73 21 04 Installation of Fuel Control Unit 4L16 73 21 05 Preparation of Fuel Control...

Page 1010: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4L6...

Page 1011: ...n regarding removal installation and checks to the various engine fuel system components not covered in this manual refer to Pratt and Whitney Engine Maintenance Manual No 3030442 Chapter 73 DISTRIBUT...

Page 1012: ...UEL PUMP 2 DISCHARGE FILTERCOVER 3 DISCHARGE FILTER ELEMENT 4 PREFORMEDPACKING 5 PREFORMEDPACKING 6 INLET FILTERCOVER 7 INLET FILTERELEMENT 8 PREFORMEDPACKING 9 PREFORMEDPACKING 10 DRIVE SHAFT Figure...

Page 1013: ...ossible danger of electrostaticdischarge Observe allfire precautions whenworking withfuel 1 Usingthe test rig setthe regulatorto zero closethe outlet valve openfillervalveand removeplug CAUTION Insure...

Page 1014: ...PLACE 13 NIPPLE 5 14 ELBOW 90 1 5 NIPPLE 2S 16 FILTER 10 MICRON ELEMENT 17 NIPPLE 2 18 TEE GAUGE TO 100 PSI 20 VALVE 2 21 NIPPLE 5 22 NIPPLE 23 PLUG 2 SEE NOTE 24 NUT 25 SCREW 26 RETAINING BRACKET ST...

Page 1015: ...r to Figure 73 3 The purpose of the fuel scavenge system is to collect residual fuel after engine shutdown and return the fuel to the nacelle fuel tank during engine start The system consists of a sol...

Page 1016: ...ble Cause Ren edy Fuel being drained overboard during engine start Fuel being drained overboard during engine shutdown Restricted jet pump nozzle Solenoid valve not opening Remove nozzle and clean Che...

Page 1017: ...order CONTROLLING FUEL CONTROL UNIT REMOVAL OF FUEL CONTROL UNIT Refer to Figure 73 4 1 Ascertain that the fire wall fuel shutoff valve is in the OFF position 2 Remove the engine cowling Refer to Chap...

Page 1018: ...tsare properlylockwiredand sealed Return the unit if there is any evidenceof tampering 2 Make sure the Py and P3 air section ports are sealed withplugs and remainso until completion of this procedure...

Page 1019: ...3 NUT 14 WASHER 15 FUEL PUMP 16 DRIVE COUPLING 17 PREFORMEDPACKING 18 NUT 19 PY LINE ELBOW 20 PREFORMEDPACKING 21 BACK UP RING 22 NUT 23 FUELOUTLET LINE ELBOW 24 PREFORMEDPACKING 25 BACK UP RING 26 FU...

Page 1020: ...ds and lock withcotter pin 6 Perform an engine motoring run with starting lever in run position PREPARATIONOF FUEL CONTROLUNIT FOR SERVICE ON ENGINE 1 Disconnectthe fuellineat the flowdivider inletand...

Page 1021: ...NCE MANUAL DO NOTADJUST CUT OFF VALVE LINKAGE ADJUSTMENT MAXIMUMNg ADJUSTMENT FUEL PUMP F C U COUPLING SPLINE HIGHIDLESTOP CUT OFF STOP ADJUST SPILLVALVE FUEL IN Figure 73 5 Fuel Control Adjustments 7...

Page 1022: ...to 64 D Rapidly less than I second move the power control lever to position marked in step B E Note and record the time required for Ng to reach 97 5 of the value recorded in step B F Immediatelyas N...

Page 1023: ...and the signal output fromthe potentiometersinthe fuel flow transmitters Integratingtheflowratefromthe twofuelflowtransmitters itsumsthesignalsanddisplaysfrom the resultson a four digit mechanicalcoun...

Page 1024: ...prevent contamination INSTALLATION OF FUEL PRESSURE TRANSMITTER 1 Position the transmitter and secure with screws 2 Remove protective caps and connect fuel linesto inlet and outlet on transmitter 3 At...

Page 1025: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 4L21 THRU 4L24 INTENTIONALLY LEFT BLANK 4L21...

Page 1026: ...MAINTENANCE MANUAL CARD 5 OF5 PA 31T3 T1040 PIPER AIRCRAFT CORPORATION PART NUMBER 761765...

Page 1027: ...or System Chapters are then broken down into Sub System Sections These sections are identifiedby the secondelement ofthe standardizednumberingsystem The number 40 ofthe basicnumber series32 40 00is fo...

Page 1028: ...RIAL NUMBERS 31T 8275001 TO 31T 8275025 INCL PA 31T T1040 1983 SERIAL NUMBERS 31T 8375001 TO 31T 8375005 INCL PA 31T T1040 1984 SERIAL NUMBERS 31T 8475001 AND UP 5A3 PIPER AIRCRAFT T 1040 MAINTENANCE...

Page 1029: ...icated by a black vertical line along the left hand margin of the frame opposite revised added or deleted material Revision lines indicate only current revisions with changes and additions to or delet...

Page 1030: ...h Electrothermal Propeller Deice Maintenance Manual P N 68 04 712 Latest Revision B F Goodrich Electrothermal Propeller Deice Installation and Removal Procedures P N 59 728 Latest Revision ENGINE PT6A...

Page 1031: ...l Models Lear Siegler Inc Overhaul Manual Series 23048 P N 8013C P N 23700 P N 23202 PIPER PUBLICATIONS PARTS CATALOG INSPECTION MANUAL 100HOLR 761 761 Piper Aircraft Corporation 820 E Bald Eagle Stre...

Page 1032: ...Sankvo Inc 10719 Sanden Dr Dallas Texas 75238 214 349 3030 Telex 73 0497 TIF Instruments 3661 N W 74th Street Miami Florida 33147 305 696 7100 Edo Corporation Avionics Division P O Box 610 Municipal...

Page 1033: ...ldsboro Road Suite 102 Bethesda Maryland 20034 301 229 5000 Leach Corporation 5915 Avalon Boulevard Los Angeles California 90003 213 232 8221 Emergency Locator Transmitter Engines Environmental System...

Page 1034: ...Marmon Division 1214 Exposition Boulevard Los Angeles California 90064 213 774 3230 Aerosonic Corporation 1212 N Hercules Avenue Clearwater Florida 33515 813 461 3000 Landing Gear Hydraulic Actuators...

Page 1035: ...tor Woodward Governor Company Drake and Lemay Roads Fort Collins Colorado 80521 303 482 5811 Auxilec Incorporated One Willow Park Center Farmingdale New York 11735 516 694 1441 Lear Siegler Incorporat...

Page 1036: ...MOORING REQUIRED PLACARDS SERVICING STANDARD PRACTICES AIRFRAME ENVIRONMENTAL SYSTEM AUTOFLIGHT COMMUNICATIONS ELECTRICAL POWER EQUIPMENT FURNISHINGS FIRE PROTECTION FLIGHT CONTROLS FUEL HYDRAULIC PO...

Page 1037: ...STRUCTURES DOORS FUSELAGE STABILIZERS WINDOWS WINGS PROPELLER STANDARD PRACTICES ENGINES POWER PLANT ENGINE TURBO PROP ENGINE FUEL SYSTEM IGNITION AIR ENGINE CONTROLS ENGINE INDICATING OIL SYSTEM STAR...

Page 1038: ...er Doors 1G11 12 9 Lubrication Chart Cabin Door Baggage Door Seats 1G12 12 10 Lubrication Chart Air Conditioner Quill Shaft 1G12 20 1 Torque Wrench Extension IHI 20 2 Correct Method of Installing Rod...

Page 1039: ...Installing Pulley and Drive Plate Bearing 2E8 21 35 Installing Pulley and Drive Plate 2E8 21 36 Removing Coil Housing Retaining Ring 2E9 21 36a Positioning Sankyo Compressor Internal Parts 2E I 21 36b...

Page 1040: ...9 Installation of Aileron Rigging Tool 2J 13 27 9a Wrapping Control Pedestal Aileron Trim Drum 2J 16 27 10 Trim Controls Installation 2J 17 27 11 Aileron Control Travels and Cable Tension 2J 18 27 12...

Page 1041: ...Pump 3C10 28 15 Test Equipment Hookup 3C15 28 16 Alternate Indicator Bench Test Hookup 3Cl8 28 17 Fuel Gauge Adjustment 3C19 29 1 Schematic Diagram Hydraulic System 3D20 29 2 Schematic of Power Pack...

Page 1042: ...Use of Dial Indicator 3H17 30 20 Centering of Brushes on Slip Rings 3H1 30 21 Wiring Schematic Electric Propeller Deicing System 3H 18 30 22 Modular Brush Assembly Wear Check 3H20 30 23 Angle of Conta...

Page 1043: ...Switch 3L16 32 27 GearWarningSwitchesInstallation 3L16 32 28 Nose GearWearLimits 3L18 32 29 Main GearWearLimits 3L21 33 1 LogoLight Assembly Adjustments 4B17 34 1 InstrumentAir SystemInstallation Typi...

Page 1044: ...alancing 4115 61 1 Propeller Installation 4122 61 2 Typical Nicks and Removal Method 4123 61 3 Propeller Governor 4J3 61 4 Propeller Synchrophaser Installation Woodward Type I 4J5 61 5 Propeller Synch...

Page 1045: ...t No 18338 00 5H9 95 2 Fabricated Tail Stand 5H10 95 3 Protective Closures Installation 5H 1 1 95 4 Fabricated Bellcrank Rigging Tool 5H12 95 5 Fabricated Aileron and Elevator Rigging Tool 5H13 95 6 F...

Page 1046: ...ted 2G21 2405 SpecificGravity Temperature Correction 2G22 2406 Capacity Ratings at Discharge Rates 2G23 2407 Electrolyte Freezing Points 2G23 2408 Circuit Load Chart 2H7 2601 Pressure Temperature Corr...

Page 1047: ...hooting Pneumatic System Pressure Gauge 4E5 3903 Troubleshooting Engine Oil Pressure Gauge 4E5 3904 Troubleshooting Fuel Pressure Gauge 4E6 3905 Troubleshooting Air Temperature Gauge 4E9 3906 Troubles...

Page 1048: ...ibration Data 5C21 7702 Digital Analog Torque Calibration Data 5C23 7703 Weston Kulite Torque Pressure Indicating System Tansducer Voltages 5C24 7901 Oil Pressure Gauge Calibration Data 5D17 9101 List...

Page 1049: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 5A24...

Page 1050: ...CHAPTER IGNITION 5B1...

Page 1051: ...k Igniter 5B6 74 21 03 Inspection of Spark Igniter 5B7 74 21 04 Installation of Spark Igniter 5B8 74 22 00 Ignition Cables 5B8 74 22 01 Removal of Ignition Cables 5B8 74 22 02 Cleaning of Ignition Cab...

Page 1052: ...9 o clock positions on the gas generator case adjacent to the fuel manifold The igniters are energized during the engine starting sequence or when in the auto mode auto ignition optional when torque f...

Page 1053: ...nand switchthe ignition and battery master switchesOFF 6 Reconnect the coupling nut of the ignition cable to the exciter box and remove the other cable coupling nut then repeat Steps 3 thru 5 7 If no...

Page 1054: ...nput connector CA UTION Do not allow ignition cable braiding or ferrules to rotate when removing coupling nuts 3 Disconnectthe two ignition cablecouplings from the output connectors on the exciter 4 R...

Page 1055: ...r plug from the gas generator case along with the copper gasket CLEANING OF SPARK IGNITER 1 Cap the cable end of the igniter plug to prevent entry of foreign material during cleaning NOTE The electrod...

Page 1056: ...OSION LIMITS C419 NEW IGNITER ACCEPTABLEWEAR WORN OUT P W PART NO 3014986 3014985 3024706 3027280 3031213 VENDOR NAME AND PART NO Champion Bendix AC Champion Bendix FHE 182 10 380700 1 5611760 CH34055...

Page 1057: ...ewingon the couplingnut 4 Insert central conductor of ignitioncable into respectivespark igniterand connect cable IGNITION CABLES The two ignition cable assembliesconsist of electrical leads contained...

Page 1058: ...with conductors may result in a high resistance path which could generate heat and oxidation 3 Apply a light film of fluorocarbon spray lubricant to any cleaned areas INSPECTION OF IGNITION CABLES 1 I...

Page 1059: ...VAL OF IGNITION CUTOFF SWITCH I Removethe topcoverplatesofthepedestal one isforward of thecontrollevers theother surrounds the levers by removing their attachment screws 2 Removethe switchfromits moun...

Page 1060: ...chinserieswitha squatswitch With the ignition switch in the AUTO OFF position the ignition willcome back on if the starter is switchedon or iftheenginetorque fallsoffto a lowvalue inflight The lowtorq...

Page 1061: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 5B12...

Page 1062: ...CHAPTER AIR 5B13...

Page 1063: ...ER AIRCRAFT T 1040 MAINTENANCE MANUAL CHAPTER 75 AIR TABLE OF CONTENTS EFFECTIVTIY CHAPTER SECTION SUBJECT GRID NO SUBJECT EFFECTIVITY 75 00 00 GENERAL 5B15 75 Cont Effec Page 1 Issued March 26 1982 5...

Page 1064: ...gair to the compressorand power turbine discs and the third providesair for the compressorbleed valvesand airframe services For a full description of the systems and their related maintenance adjustme...

Page 1065: ...CHAPTER ENGINECONTROLS...

Page 1066: ...lever Adjustment 5B24 76 13 03 Throttle Control Cable to Power Lever Arm Adjustment 5CI 76 14 00 Propeller Pitch Control Lever 5C2 76 14 01 Propeller Pitch Control Lever Adjustment 5C2 76 14 02 Beta...

Page 1067: ...the fuel control to the flow divider and dump valve assembly for fuel flowingto the primary and secondary fuel nozzles As a secondfunction the condition leveroperates oneof the two switchesnecessaryfo...

Page 1068: ...18 PROPELLERGOVERNORAIR PRESSURETUBE Py 19 PUSH PULLCONTROL WIRE ROPE 20 CENTERFIRESEAL MOUNT RING 21 LOW PITCHSTOPADJUSTER 22 PROPELLERGOVERNOR INTER CONNECTROD 23 PROPELLERSPEEDSELECTLEVER MAX STOP...

Page 1069: ...ION 750 2 stamped 1 75 betweenholes REVERSE DEAD BAND 525 527 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 49 36 LEVERARM A DIMENSION 1 437 01 34 35 SKETCHB SKETCH C NOTE 603 START CONTROL ARM DELETEDFOR...

Page 1070: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 529 Figure 76 1 Engine Controls cont 76 11 01 Page 76 04 5B21 Issued March26 1982...

Page 1071: ...e followingchecks A Forward gas generator Ng pickup dead band B Power lever alignment check C Reverse maximum power setting D Check that maximum Ng Speed Adjustment contacts part power trim stop 11 If...

Page 1072: ...e Handling Procedure ENGINE CONTROL ADJUSTMENTS The following engine control adjustments are preliminary adjustments After these adjustments are complete the engine power adjustments must be checked N...

Page 1073: ...h engineshave the same length lever Refer to the Parts Catalog 7 Position the power lever input arm 90 degrees from the pivot pins Refer to Figure 76 1 Sketch A Place bolt through lower end of arm and...

Page 1074: ...that when the fuelcontrol unit input arm isat the 22 5degreeposition the rod end bearingof the fuelcontrol unit interconnectrodjust alignswith the top hole of the fuel control unit actuating lever The...

Page 1075: ...barrel inor out to adjust the pistonflush withthecap nut Remember tokeepcheckingflushfit whileholdingforwardpressureon linkage Afteradjustingthe betavalve tighten and safetythe barrel and jam nut LOW...

Page 1076: ...CH STOPSWITCH BETA 8 PROPELLERREVERSINGLEVER 9 SPRING 10 FEEDBACKRING 11 BRACKET 12 CARBON BLOCK 13 ADJUSTING BOLT 14 BRUSH BLOCK RETAINER 15 BRACKET PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 519 TORQU...

Page 1077: ...ESWITCH ADJUSTMENT Refer to Figure 76 1 The propellerreverseswitchismounted on the rearpropellerreverselinkageand isactuated bymovement of the propeller control cam in the reverse direction Adjust the...

Page 1078: ...is provided to record data obtained during the adjustment procedure Refer to Chart 7601 Before attempting any power adjustments check to be certain the engine controls are properly rigged NOTE All en...

Page 1079: ...EET NOMINAL SETTINGS IDLE Ng 52 MIN IDLE ITT 6 60 C MAX OIL PRESSURE 40PSI MIN IDLE 80TO 100 PSI TAKI OIL TEMP 0 C to 99 0 C FUEL PRESSURE 15 to 35 psi MAX PROPELLER SPEED 2200 RPM REVERSE MAY POWER G...

Page 1080: ...1 Holding track point position on thecam control lever insert tool P N 51516behindthe cam ontothe pinandholdthe camandtool inpositionwithasmallpair ofvisegrippliers Install visegrip plierstight enoug...

Page 1081: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL CHART 7602 2000RPM TORQUE CURVE 534 PRESSURE ALTITUDE FT PROP TORQUE AT 2000RPM LB FT 76 16 00 Page 76 15 Added November 15 1982 5C8...

Page 1082: ...greaterthan the minimum fuelflow setting At higheraltitudesthe minimum fuel flow setting willgovern Ng idle speed CAUTION The minimum fuelflow setting is NOT FIELD adjustable NOTE Do not attempt idle...

Page 1083: ...NMENT CHECK CAUTION The wheels should be chocked and the parking brakes set when applying power in excess of 600foot pounds as the aircraftcould move A Advance the power levers to 400 600 800 and 1 00...

Page 1084: ...KETCHA 1 5 2 PROPELLER GOVERNOR 1 ACCELERATION ADJUSTMENT 2 P1 PRESSURE PORT 3 THROTTLE LEVER 4 IDLE SPEED ADJUSTING SCREW 5 MAXIMUM SPEED ADJUSTMENT 6 PX PRESSURE PORT 7 CUTOFF LEVER 8 FUEL INLET 9 F...

Page 1085: ...rsepower use the followingequation Q x Np x 0 00019 This equation will givethe reversepower for the prevailingambient conditions E If necessary adjust the reverse stop on the power lever linkage Refer...

Page 1086: ...GROUND PERFORMANCE CHECK Engine performance checking cur es enable engine performance to bechecked on the ground over a wide range of ambient temperatures whilereducing the likelihood of an overtorqu...

Page 1087: ...400 T 1040 MAINTENANCE MANUAL CHART 7603 FUEL FLOW 105 z 95 30 20 10 0 10 20 30 40 50 60 65 90 40 OAT C 76 17 01 Page 76 21 Issued March 26 1982 5C14...

Page 1088: ...600 500 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL CHART 7605 INTER TURBINE TEMPERATURE OAT C CHART 7606 TORQUE 1200 1100 1000 900 800 600 500 400 76 17 01 Page 76 22 Issued March 26 1982 5C15...

Page 1089: ...ature check instrumentation It isnormalfor thefuelflow ITTandNg to bebelowthechartvalue but shouldnot exceedit 7 If engine performance deviates from the preceding limits refer to Pratt and Whitney Eng...

Page 1090: ...CHAPTER ENGINE INDICATING 5C17...

Page 1091: ...stem Description Calibration Torque Pressure Indicating System Weston Kulite Description System Calibration Test Torquemeter Transducer Test Weston Kulit Tachometer Generators Propeller and Gas Genera...

Page 1092: ...g system as follows 1 Remove the torque pressure transducer from the reduction gear box case 2 Connect a suitable pressure test unit with a calibrated gauge to the pressure transducer using appropriat...

Page 1093: ...RCRAFT T 1040 MAINTENANCE MANUAL C449 Figure 77 1 Torque System Calibration Bendix THIS SPACE INTENTIONALLY LEFT BLANK Effectivity Bendix Torque Indicating System 77 11 02 Page 77 02 Revised March 5 1...

Page 1094: ...re tester to 22 9 psiand adjust lowsetting on gauge to 700foot pounds Apply 39 25psi and adjust high setting to 1200 foot pounds 5 After making the Low L and High H adjustments on the indicator rechec...

Page 1095: ...C power source 6 Increase pressure to the transmitter to 50 psi and check reading Readings must remain in the tolerances as specified in Chart 7702 7 If necessary adjust the gauge to obtain the corre...

Page 1096: ...Torque Calibration CHART 7702 D ITAL ANALOG TORQUE CALIBRATION DATA TEST UNIT PS1 0 5 10 15 20 25 30 35 40 45 50 55 60 DIGITAL DISPLAY PS50154 3 BLANK 153 306 458 611 764 917 1070 1223 1376 1528 1681...

Page 1097: ...is tested and found to be servicable The torque pressure gauge should be replaced CHART 7703 WESTON KULITE TORQUE PRESSURE INDICATING SYSTEM TRANSDUCER VOLTAGES PSIG 0 5 10 15 20 25 30 35 40 45 50 55...

Page 1098: ...haft splines with Molybdenum Disulfide Type G paste form lubricant MIL G 21164 6 With the electrical socket pointing down slide the generator into placeover the mounting studs 7 Secure the unit in pla...

Page 1099: ...ld be between 0 58 and 0 74 ohms CA UTION The thermocouples will generate a small potential which will produce errors in the measured values if this check ismade while the engine is hot NOTE If severa...

Page 1100: ...resistance of the aircraft harness with the engine harness disconnected and the red and yellow wires temporarily bolted together instead of connected to the ITT indicator terminals The values should b...

Page 1101: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL Temperature mv Millivolts Tolerance 77 21 01 Page 77 10 5D4...

Page 1102: ...ield Instrument function switch to Indicate and the Digital Multimeter to DCV and I position 4 Check the ITT gauge for each temperature indication by the following A While pressing the test switch and...

Page 1103: ...CHAPTER OIL SYSTEM 5D6...

Page 1104: ...Cooler Installation of Oil Cooler Oil Filter Element Maintenance Oil Cooler Exhaust Door Removal of Oil Cooler Door Transmission Cleaning Inspection and Repair of Oil Cooler Door Transmission Installa...

Page 1105: ...l cooler duct 4 Disconnect the oil cooler inlet and outlet lines at the oil cooler and cap the lines to prevent contamination 5 Drain the oil cooler 6 Removethe attachment hardware connectingthe coole...

Page 1106: ...CTIONCASE SCAVENGE PUMP 18 POWER TURBINEBEARINGS SCAVENGE PUMP 19 ACCESSORYCASE SCAVENGEPUMP 20 BYPASS VALVE 21 NO 2 SCAVENGE PUMP 22 DRAIN TO ACCESSORYGEARBOX 23 OIL TANK DRAIN 24 FILTERBYPASS VALVE...

Page 1107: ...LET HOSE 3 OIL COOLER OUTLET HOSE 4 OIL COOLER OUTLET 5 OIL COOLER INLET 6 SUPPORTFOR DRAIN LINES 7 OIL COOLER NUT PLATE ASSEMBLY 8 OIL COOLER INLET HOOD ASSEMBLY 9 MACHINE SCREW AND LOCK WASHER Figur...

Page 1108: ...heelementfor cloggedpassagesand broken wires If more than fivepercentof the element remains cloggedafter cleaning return to an overhaul facility If dents or broken wires are found replacethe element N...

Page 1109: ...pliers vise grips using a light pressure on the transmission screw shaft Refer to Figure 79 4 C Rotate the screw shaft by moving the pliers A slight movement should be felt but not to exceed 312 5 16...

Page 1110: ...RODEND 4 JAM NUT 5 SPRING 6 SPACER 7 SEAL 8 TRANSMISSION ASSEMBLY 9 FIREWALL 10 BOLTASSEMBLY 11 SETSCREW 12 SWITCH 13 HINGEASSEMBLY 14 TRANSMISSION SCREW SHAFT 15 TRANSMISSION SLEEVE 16 BRAKESOLENOID...

Page 1111: ...h a completeopening and closingcycle OIL TO FUEL HEATER Refer to Figure 79 5 The oil to fuelheater isa heat exchangerwhichusesheatfromtheenginelubricatingoilsystemto preheat the fuel for the fuel syst...

Page 1112: ...Position oil to fuelheater on studs of flange on accessorygear box 3 Insertsmallerdiameter end of checkvalvethrough large holeof rearliftingbracketandinto bossor mating flange of heater 4 Insertlarged...

Page 1113: ...CK UP RING 8 PLAIN HEX NUT 9 ELBOW 10 PREFORMEDPACKING 11 OIL RETURNCHECKVALVE 12 RETAINING PLATE 13 PREFORMEDPACKING 14 MACHINGE BOLT 8 NOTE TORQUEFUELOUTLETHOSECOUPLING NUT270 300 IN LBS TORQUE COUP...

Page 1114: ...gauge reading 8 Turn handle counterclockwisefor a low pressure of 105psi 9 Again comparetest gauge reading with oil pressure gauge reading NOTE Test gaugemay need tapping to reducefrictional errors 10...

Page 1115: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 5D18...

Page 1116: ...CHAPTER STARTING 5D19...

Page 1117: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL FOR INFORMATION ON THE STARTER GENERATOR REFER TO CHAPTER 24 ELECTRICAL POWER 5D20...

Page 1118: ...CHAPTER CHARTS AND WIRING DIAGRAMS 5D21...

Page 1119: ...91 00 03 91 00 04 91 00 05 91 00 06 91 00 07 91 10 00 GENERAL Consumable Materials Torque Requirements Lubrication of Threads Lubrication of Gaskets and Seals Conversion Charts Decimal Millimeter Equ...

Page 1120: ...ichare applicableto variouschaptersandsystemscovered in this manual Allelectrical schematicsare also includedin this chapter CONSUMABLEMATERIALS Refer to back of Consumable Materials List for Vendor I...

Page 1121: ...i Galling Solution MIL A 907 Ease Off Taxacone Company MIL T 5544 Armite Product Anti Seize Compound Royco 44 Armite Laboratories Exxon Oil Company Royal Lubricants Co Armite Laboratories Fel Pro Inco...

Page 1122: ...Service Bulletin No 12044 Solarite 400 MIL G 23827A See Note 1 MIL G 3278 Permatex No 2 2196 74 1 Supermil Grease No A72832 Rovco 27A Shell 6249 Grease RR 28 Castrolease A Low Temp Grease E P 5114 E...

Page 1123: ...501 Daring Grease 2 XSG 6152 Code 71 502 Alvania Grease 2 XSG 6151 Code 71 012 Cyprina Grease 3 XSG 6280 Code 71 003 Shell Oil Corporation Royal Lubricants Company Sinclair Refining Co California Tex...

Page 1124: ...lux Mobil Oil Corporation EP2 Royco 45A Royal Lubricants Co L 1231 Sinclair Refining MIL G 7711 MIL G 21164 MIL G 6032 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL Regal AFB2 Regal Starfak Premium PED 304...

Page 1125: ...n diameter 3 in long MIL H 5606 Univis 40 Aero Lubr Brayco 756D TL 5874 PED 3565 Aircraft Hydraulic Oil AA iplate Fiske Brothers Refining Company vdraulic 6D Sears Roebuck and Company or most hardware...

Page 1126: ...d HV Fed Spec TT M 261 MIL M 7866 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL Oil Air Conditioner Oil Lubricating General Purpose Low Temperature Molykote Tvpe G Paste Molykote Type 2 Powder Frigidaire 5...

Page 1127: ...in VENDOR Unelco Corporation Wooster Products Incorporated Products Research Company CEE BEE Chemical Co RS 24b Stripper thick PR 1422 A 2 Sealant Brushing Consistency Products Research Company PR 142...

Page 1128: ...T VENDOR Sealing Compound Gasket and Joint Sealer Tite Seal PR 1321 B 1 2 Radiator Specialty Co Products Research Company DC 4 DC 6 Compound G 624 Methylethylketone Methylene Chloride Acetone Y2900 Do...

Page 1129: ...T 27730 Permacel 412 Johnson Johnson Inc or High Pressure Permacel Division Oxygen System Vinyl Foam I in x in 530 Series Type I Norton Tape Division Vinyl Foam Tape in x 1 in 501 Series Type 11 Nort...

Page 1130: ...g Avenue Canoga Park California 91304 DuPont Company Finishes Div Dupont Bldg Wilmington Delaware 19898 302 774 1000 E Exxon Oil Company 1251 Avenue of the Americas New York New York 10019 212 757 120...

Page 1131: ...400 N Lexington Avenue Pittsburgh PA 15208 412 247 3000 Royal Lubricants Company River Road Hanover New Jersey 07936 201 887 3100 S Shamban W S and Co 11543W Olympic Blvd Los Angeles CA 90064 213 879...

Page 1132: ...inia Chemical 3340 W Norfolk Rd Portsmouth Va 23703 804 484 5000 Wooster Products Inc 30 Spruce Street Wooster Ohio 44691 216 262 8065 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL CHART 9101 LIST OF CONSU...

Page 1133: ...102 lists the torque values for flared fittings of various sizes and material NOTE Whenflared fittings are being installed ascertain that the male threads areproperly lubricated Torque the fittings in...

Page 1134: ...Chart 9103 This is referredto asfinal torque which should registeron the indicator or the setting for a snapover typewrench NOTE For more detailson torquing refer to FAA Manual AC43 13 1 BOLT SIZE NUT...

Page 1135: ...315 AN 363 AN 365 NAS 1021 MS 17825 MS 21045 MS 20365 MS 20600 NAS 679 AN 320 AN 364 NAS 1022 MS 17826 MS 20364 AN 310 AN 315 AN 363 AN 365 MS 17825 MS 20365 MS 21045 NAS 1021 NAS 679 NAS 1291 AN 320...

Page 1136: ...ads on tapered fittings Apply the lubricant to the next three threads only 6 Ascertain that lubricant does not enter fittings or flared areas 7 Any fittings going to the engine should be lubricated wi...

Page 1137: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL CHART 9105 DECIMAL CONVERSION 91 00 05 Page 91 18 Issued March 26 1982 5E16...

Page 1138: ...PIPER AIRCRAFT T 1040 MAINTENANCEMANUAL CHART 9106 TORQUE CONVERSION INCH POUNDS TO CENTIMETER KILOGRAMS cmkg 50 cmkg 100cmkg 150cmkg 200 cmkg 250 cmkg...

Page 1139: ...3 Procedure for Converting Inchesto Millimeters Refer to Chart 9107 A Example Convert 1 5inchesto millimeters 1 Read down inchescolumn to 1 inches 2 Read across top inch column to 0 5 3 Read down and...

Page 1140: ...S MILS MM YARDS M KG BTU KW HR DRAM CU CM CU IN U S GAL LITERS CU IN CU FT U S GAL LIQ LITERS CU IN CU FT LITERS IMPERIAL GAL FLUID OZ CM FT BTU FT LB KILOGRAMS LITERS METERS METER KILOGRAM OUNCES AVD...

Page 1141: ...130 140 150 160 170 180 190 200 210 F 94 0 76 0 58 0 40 0 22 0 4 0 14 0 32 0 50 0 68 0 86 0 104 0 122 0 140 0 158 0 176 0 194 0 212 0 230 0 248 0 266 0 284 0 302 0 320 0 338 0 356 0 374 0 392 0 410 0...

Page 1142: ...133 2 387 1 397 1 651 1 905 2 159 2 413 1 422 1 676 1 930 2 184 2 438 1 447 1 701 1 955 2 209 2 463 1 473 1 727 1 981 2 235 2 489 1 498 1 752 2 006 2 260 2 514 INCHES 0 0 0 1 0 2 0 3 0 4 0 00 0 01 0...

Page 1143: ...2 2 8194 2 794 2 7781 2 7051 26416 2 5781 51 0067 52 00635 1 16 00625 53 00595 54 0055 55 0052 3 64 00468 56 00465 57 0043 58 0042 59 0041 60 0040 61 0039 62 0038 63 0037 1 7018 1 6129 1 5875 1 5113 1...

Page 1144: ...ECTOR NUMBER S AND LOCATIONS CIRCUITS AUTOPILOT E 100 Series Left Wing and Nacelle CONTROL SURFACE FLIGHT INSTRUMENT LANDING GEAR HEATER VENTILATING DEICING E 200 Series Right Wingand Nacelle E 300 Se...

Page 1145: ...SWITCH TYPE PUSH TYPE PUSH PULL TYPE THERMAL SWITCH BEACON ELECTRICAL CLUTCH TERMINAL BLOCK RESISTOR CONNECTORS KNIFE DISCONNECT SHIELDED CONDUCTORS CONDUCTORS PUSH BUTTON SWITCH INSULATED CONNECTOR C...

Page 1146: ...Heat and Control Optional 5G15 ELECTRICAL SYSTEMS Bus Main Power Dist Batt Ext Pwr Nicad Optional 5F7 3 Starter Generator Left 5F9 4 Starter Generator Right 5F11 21 Emergency Locator Transmitter E L T...

Page 1147: ...ers Gas Generator Propeller Left and Right 5G19 20 Torque Meters 19 21 Turn and Bank Electric Optional 5 Voltmeter 5F LANDING GEAR 15 Gear Left Right Solenoid and Warning 5G9 1 Landing Gear Safety Swi...

Page 1148: ...SHEET NO SCHE MATIC GRID NO 13 9 19 9 WARNING SYSTEMS See Annunciators Baggage Door Ajar Fire Detection Left Right Optional Nose Cone Stall Vane Horn A O G Switch and Time Delay Windshield Wiper 5G5 5...

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Page 1162: ......

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Page 1175: ...CHAPTER SPECIALPURPOSE EQUIPMENT 5H7...

Page 1176: ...AL PURPOSE EQUIPMENT TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION SUBJECT 95 00 00 GRID NO S UBJIECT EFFECTIV ITY GENERAL 5H9 95 10 00 95 11 00 TOOLS AND TEST EQUIPMENT Construction of Tire Balancer...

Page 1177: ...CRAFT T 1040 MAINTENANCE MANUAL GENERAL This chapter contains illustrations of the variousfabricated and purchasedspecialtools whichmay be required when performing various forms of maintenance on the...

Page 1178: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 101 375 HOLE 75 R TYP I Figure 95 2 Fabricated Tail Stand 95 10 00 Page 95 02 Issued March26 1982 5H10...

Page 1179: ...STUB PLUG 51456 00 2 PROPELLERANTI SPIN BRACE 82069 2 3 ENGINE AIR INLETCOVER 82082 2 4 ENGINE GROUND PROTECTIONCABLE 51461 02 5 GROUND PROTECTIONWARNING STRAP 51526 00 Figure 95 3 Protective Closures...

Page 1180: ...MATERIAL 25T0 50 ALUMINUM ORSTEEL 9 10 00 Page 95 04 Issued March 26 1982 5H12...

Page 1181: ...bricated Aileron and Elevator Rigging Tool PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 199 DRILLANDTAP INCH BOLT FILE TOLENGTH 31 625 PLACETHISSIDE NEXTTo ELEVATOR 25 141 14 625 50 to 1 0 DRILLANDTAP INC...

Page 1182: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 1201 Figure 95 6 Fabricated Rudder Rigging Tool 95 10 00 Page 95 06 Issued March 26 1982 5H14...

Page 1183: ...95 10 00 Page 95 07 Issued March26 1982 5H15...

Page 1184: ...Figure 95 8 Fabricated Tool Checking Nose Gear Link Travel 95 10 00 Page 95 08 5H16 Issued March 26 1982 5H16...

Page 1185: ...96 NOTE ITIS IMPORTAN CENTER LINE ACCURACY BEUSED WHEN LOCATING HOLES FOR INSTALLATION OFBUSHING SIGHT SLOT AND ELONGATED HOLE Figure 95 9 Fabricated Tool Checking Main Gear Side Brace Link Travel 95...

Page 1186: ...T 1040 MAINTENANCE MANUAL 218 TOP SIDE MATERIAL HARD WOOD 1 10 x 1 x 11 56 NOTE MARK LARGE END FORWARD Figure 95 10 Fabricated Tool Checking Main Gear Toe In Adjustment 95 10 00 Page 9510 5H18 Revised...

Page 1187: ...uring with a washer and nut a drill press and file may be used to make the off set on the bushing The turned down part shouldjust slide inside the bearing race Ream the pilot hole to slide over the 8...

Page 1188: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 1094 Figure 95 12 Fabricated Tool Checking Nose Wheel Alignment 95 11 00 Page 95 12 Issued March 26 1982 5H20...

Page 1189: ...RING KNURL THREAD 1 2 x 20 PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL C710 6 00 II I I II II II II Figure 95 13 Fabricated Test Fitting Emergency Gear Extension System 95 11 00 Page 95 13 Added August4...

Page 1190: ...STION HEAD OPENING RUBBER STOPPER DRILL OUT TO NECESSARY DIA CLAMP SEAL CAP Figure 95 14 Suggested Design for Seal Plate Plugs and Caps for Combustion Leakage Test THIS SPACE INTENTIONALLY LEFT BLANK...

Page 1191: ...48 50 AND POLISH CONTOUR AREA FREE OF TOOL MARKS 5 TO 10 RMS AFTER HND 3 SERVICE GYIIA GY18B RIVETS SEMI TUBULAR RIVETS 4 EDGE OF FORMING TOOL MUST BE ON CENTER LINE OF PEEN AS SHOWN WHEN FORMING CONT...

Page 1192: ...1345 95 11 00 Page 95 16 Issued March 26 1982 5H24...

Page 1193: ...MANUAL TURBINETEMPERATURE INDICATINGTEST SET 494 BARFIELDINSTRUMENTCORPORATION MODEL 2312G TORQUE METERPRESSURETESTER MODEL 2311F BARFIELD INSTRUMENTCORPORATION Figure 95 16 Special Tools cont 95 11...

Page 1194: ...SHARP EDGE LARGE SEALANT CUTTING TOOL BEVELED SURFACE SHARP EDGE SEALANT REMOVAL TOOL SMALL SEALANT CUTTING TOOL 0 04 APPROX SEALANT FAIRING TOOL SMALL SEALANT FAIRING TOOL WITH SPOON TYPE HEAD LARGE...

Page 1195: ...R MANUFACTURER DATAPRECISION SUPPLIER Q E D COMPANY 2916 FEDERAL STREET CAMDEN NEWJERSEY 08105 Figure 95 16 Special Tools cont PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL 498 95 11 00 Page 95 19 Issued M...

Page 1196: ...535 BROAD HOLLOW ROAD MELLVILLE N Y 11747 TOOL P N E3390 AUXILEC INC 535 BROAD HOLLOW ROAD MELLVILLE N Y 11747 KEYP N E3392 AUXILEC INC 535 BROAD HOLLOW ROAD MELLVILLE NY 11747 TOOL P N E3370 AUXILECI...

Page 1197: ...PIPER AIRCRAFT T 1040 MAINTENANCE MANUAL GRIDS 515THRU 5L24 INTENTIONALLY LEFT BLANK 515...

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